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		<summary type="html">&lt;p&gt;PenelopRosenste: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;A &#039;&#039;&#039;biaxial nematic&#039;&#039;&#039; is a spatially homogeneous [[liquid crystal]] with three distinct optical axes. This is to be contrasted to a simple [[nematic]], which has a single preferred axis, around which the system is rotationally symmetric. The [[symmetry group]] of a biaxial nematic is &amp;lt;math&amp;gt;D_{2h}&amp;lt;/math&amp;gt; i.e. that of a rectangular right parallelepiped, having 3 orthogonal &amp;lt;math&amp;gt;C_2&amp;lt;/math&amp;gt; axes and three orthogonal mirror planes. In a frame co-aligned with optical axes the second rank [[order parameter]] [[tensor]] of a biaxial nematic has the form &lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
Q=&lt;br /&gt;
\begin{pmatrix}&lt;br /&gt;
-\frac{1}{2}S+T &amp;amp; 0 &amp;amp;0 \\&lt;br /&gt;
0 &amp;amp;-\frac{1}{2}S-T &amp;amp; 0 \\&lt;br /&gt;
0 &amp;amp; 0&amp;amp; S\\&lt;br /&gt;
\end{pmatrix} &lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
where &lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;S&amp;lt;/math&amp;gt; is the standard nematic scalar order parameter&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;T&amp;lt;/math&amp;gt; a measure of the biaxiality. &lt;br /&gt;
&lt;br /&gt;
The first report of a biaxial nematic appeared in 2004&amp;lt;ref&amp;gt;&lt;br /&gt;
{{cite journal&lt;br /&gt;
 |last1=Madsen |first1=L. A.&lt;br /&gt;
 |last2=Dingemans |first2=T. J.&lt;br /&gt;
 |last3=Nakata |first3=M.&lt;br /&gt;
 |last4=Samulski |first4=E. T.&lt;br /&gt;
 |year=2004&lt;br /&gt;
 |title=Thermotropic Biaxial Nematic Liquid Crystals&lt;br /&gt;
 |journal=[[Physical Review Letters]]&lt;br /&gt;
 |volume=92 |pages=145505&lt;br /&gt;
 |doi=10.1103/PhysRevLett.92.145505 |pmid=15089552 |bibcode=2004PhRvL..92n5505M&lt;br /&gt;
 |issue=14&lt;br /&gt;
}}&amp;lt;/ref&amp;gt;&amp;lt;ref&amp;gt;&lt;br /&gt;
{{cite journal&lt;br /&gt;
 |last1=Prasad |first1=V.&lt;br /&gt;
 |last2=Kang |first2=S.-Woong&lt;br /&gt;
 |last3=Suresh |first3=K. A.&lt;br /&gt;
 |last4=Joshi |first4=Leela&lt;br /&gt;
 |last5=Wang |first5=Qingbing&lt;br /&gt;
 |last6=Kumar |first6=Satyendra&lt;br /&gt;
 |year=2005&lt;br /&gt;
 |title=Thermotropic Uniaxial and Biaxial Nematic and Smectic Phases in Bent-Core Mesogens&lt;br /&gt;
 |journal=[[Journal of the American Chemical Society]]&lt;br /&gt;
 |volume=127 |pages=17224&lt;br /&gt;
 |doi=10.1021/ja052769n&lt;br /&gt;
 |issue=49&lt;br /&gt;
}}&amp;lt;/ref&amp;gt;  based on a [[boomerang]] shaped [[oxadiazole]] &#039;&#039;&#039;bent-core mesogen&#039;&#039;&#039;. The biaxial nematic phase for this particular compound only occurs at temperatures around 200 °C and is preceded by as yet unidentified [[smectic]] phases.&lt;br /&gt;
&lt;br /&gt;
[[Image:Biaxialnematic.gif|center|Biaxial nematic boomerang liquid crystal]]&lt;br /&gt;
&lt;br /&gt;
It is also found that this material can segregate into [[Chirality (chemistry)|chiral]] domains of opposite handedness.&amp;lt;ref&amp;gt;&lt;br /&gt;
{{cite journal&lt;br /&gt;
 |last1=Görtz |first1=V.&lt;br /&gt;
 |last2=Goodby |first2=J. W.&lt;br /&gt;
 |year=2005&lt;br /&gt;
 |title=Enantioselective segregation in achiral nematic liquid crystals&lt;br /&gt;
 |journal=[[Chemical Communications]]&lt;br /&gt;
 |pages=3262&lt;br /&gt;
 |doi=10.1039/B503846D&lt;br /&gt;
 |issue=26&lt;br /&gt;
}}&amp;lt;/ref&amp;gt; For this to happen the boomerang shaped molecules adopt a helical superstructure.&lt;br /&gt;
&lt;br /&gt;
In one azo bent-core mesogen a thermal transition is found from a uniaxial N&amp;lt;sub&amp;gt;u&amp;lt;/sub&amp;gt; to a  biaxial nematic N&amp;lt;sub&amp;gt;b&amp;lt;/sub&amp;gt; mesophase,&amp;lt;ref&amp;gt;&lt;br /&gt;
{{cite journal&lt;br /&gt;
 |last1=Prasad |first1=V.&lt;br /&gt;
 |last2=Kang |first2=S.-W.&lt;br /&gt;
 |last3=Suresh |first3=K. A.&lt;br /&gt;
 |last4=Joshi |first4=L.&lt;br /&gt;
 |last5=Wang |first5=Q.&lt;br /&gt;
 |last6=Kumar |first6=S.&lt;br /&gt;
 |year=2005&lt;br /&gt;
 |title=Thermotropic Uniaxial and Biaxial Nematic and Smectic Phases in Bent-Core Mesogens&lt;br /&gt;
 |journal=[[Journal of the American Chemical Society]]&lt;br /&gt;
 |volume=127 |pages=17224&lt;br /&gt;
 |doi=10.1021/ja052769n&lt;br /&gt;
 |issue=49 &lt;br /&gt;
}}&amp;lt;/ref&amp;gt; as predicted by theory and simulation.&amp;lt;ref&amp;gt;&lt;br /&gt;
{{cite journal&lt;br /&gt;
 |last1=Bates |first1=M.&lt;br /&gt;
 |last2=Luckhurst |first2=G.&lt;br /&gt;
 |year=2005&lt;br /&gt;
 |title=Biaxial nematic phases and V-shaped molecules: A Monte Carlo simulation study&lt;br /&gt;
 |journal=[[Physical Review E]]&lt;br /&gt;
 |volume=72 |pages=051702&lt;br /&gt;
 |doi=10.1103/PhysRevE.72.051702&lt;br /&gt;
|bibcode = 2005PhRvE..72e1702B&lt;br /&gt;
 |issue=5 }}&amp;lt;/ref&amp;gt; This transition is observed on heating from the N&amp;lt;sub&amp;gt;u&amp;lt;/sub&amp;gt; phase with [[Polarizing optical microscopy]] as a change in [[Schlieren texture]] and increased light transmittance and from [[x-ray diffraction]] as the splitting of the nematic reflection. The transition is a [[Phase transition|second order transition]] with low energy content and therefore not observed in [[differential scanning calorimetry]]. The positional order parameter for the uniaxial nematic phase is 0.75 to 1.5 times the mesogen length and for the biaxial nematic phase 2 to 3.3 times the mesogen length.&lt;br /&gt;
&lt;br /&gt;
[[Image:Biaxialnematic2005.png|center|600px|Azo bent-core mesogen thermal transitions in °C: K 82.8 Sy 93.4 Sx 104.3 Sc 118.5 Nb 149 Nu 176.5 I]]&lt;br /&gt;
&lt;br /&gt;
Another strategy towards biaxial nematics is the use of mixtures of classical rodlike mesogens and disklike [[discotic]] mesogens.  The biaxial nematic phase is expected to be located below the minimum in the rod-disk phase diagram. In one study&amp;lt;ref&amp;gt;&lt;br /&gt;
{{cite journal&lt;br /&gt;
 |last1=Apreutesei |first1=D.&lt;br /&gt;
 |last2=Mehl |first2=G. H.&lt;br /&gt;
 |year=2006&lt;br /&gt;
 |title=Completely miscible disc and rod shaped molecules in the nematic phase&lt;br /&gt;
 |journal=[[Chemical Communications]]&lt;br /&gt;
 |pages=609&lt;br /&gt;
 |doi=10.1039/b512120e&lt;br /&gt;
 |issue=6&lt;br /&gt;
}}&amp;lt;/ref&amp;gt; a miscible system of rods and disks is actually found although the biaxial nematic phase remains elusive.&lt;br /&gt;
&lt;br /&gt;
==See also==&lt;br /&gt;
* [[Chromonic]]&lt;br /&gt;
* [[Liquid crystal]]&lt;br /&gt;
* [[Liquid crystal display]]&lt;br /&gt;
* [[Liquid crystal polymer]]&lt;br /&gt;
* [[Lyotropic liquid crystal]]&lt;br /&gt;
* [[Plastic crystallinity]]&lt;br /&gt;
* [[Smart glass]]&lt;br /&gt;
* [[Thermochromics]]&lt;br /&gt;
&lt;br /&gt;
== References ==&lt;br /&gt;
{{reflist}}&lt;br /&gt;
&lt;br /&gt;
[[Category:Phases of matter]]&lt;br /&gt;
[[Category:Crystallography]]&lt;br /&gt;
[[Category:Liquid crystals]]&lt;/div&gt;</summary>
		<author><name>PenelopRosenste</name></author>
	</entry>
	<entry>
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		<title>Main Page</title>
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		<updated>2014-08-13T07:10:15Z</updated>

		<summary type="html">&lt;p&gt;PenelopRosenste: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;A &#039;&#039;&#039;catch-22&#039;&#039;&#039; is a [[paradoxical]] situation from which an individual cannot escape because of contradictory rules.&amp;lt;ref&amp;gt;{{cite journal | title=Catch-22 | journal=Random House&lt;br /&gt;
 Dictionary | publisher=Random House | year=2012 | url=http://dictionary.reference.com/browse/catch-22}}&amp;lt;/ref&amp;gt;&amp;lt;ref name=OALD&amp;gt;&amp;quot;[http://oald8.oxfordlearnersdictionaries.com/dictionary/catch-22 Catch 22]&amp;quot;, &#039;&#039;Oxford Advanced Learners&#039; Dictionary&#039;&#039;, accessed 16 August 2013.&amp;lt;/ref&amp;gt; Catch-22s often result from rules, regulations, or procedures that an individual is subject to but has no control over. One connotation of the term is that the creators of the &amp;quot;Catch-22&amp;quot; have created arbitrary rules in order to justify and conceal their own abuse of power.&lt;br /&gt;
== Origin and meaning ==&lt;br /&gt;
&lt;br /&gt;
[[Joseph Heller]] coined the term in his 1961 novel &#039;&#039;[[Catch-22]]&#039;&#039;, which describes absurd bureaucratic constraints on soldiers in World War II. The term is introduced by the character Doc Daneeka, an army psychiatrist who invokes &amp;quot;Catch 22&amp;quot; to explain why any pilot requesting mental evaluation for insanity—hoping to be found not sane enough to fly and thereby escape dangerous missions—demonstrates his own sanity in making the request and thus cannot be declared insane.&amp;lt;ref&amp;gt;Scriptures for a Generation: What We Were Reading in the &#039;60s - Page 162 Philip D. Beidler - 1995 &amp;quot;It is Catch-22: Doc Daneeka explains how anybody who is crazy has a right to ask to be removed from combat status but how anybody who asks is&amp;quot;&amp;lt;/ref&amp;gt;&lt;br /&gt;
{{quotation|&amp;quot;You mean there&#039;s a catch?&amp;quot;&lt;br /&gt;
&amp;lt;p&amp;gt;&lt;br /&gt;
&amp;quot;Sure there&#039;s a catch&amp;quot;, Doc Daneeka replied. &amp;quot;Catch-22. Anyone who wants to get out of combat duty isn&#039;t really crazy.&amp;quot;&lt;br /&gt;
&amp;lt;p&amp;gt;&lt;br /&gt;
There was only one catch and that was Catch-22, which specified that a concern for one&#039;s own safety in the face of dangers that were real and immediate was the process of a rational mind. [[Orr (Catch-22)|Orr]] was crazy and could be grounded. All he had to do was ask; and as soon as he did, he would no longer be crazy and would have to fly more missions. Orr would be crazy to fly more missions and sane if he didn&#039;t, but if he was sane, he had to fly them. If he flew them, he was crazy and didn&#039;t have to; but if he didn&#039;t want to, he was sane and had to. Yossarian was moved very deeply by the absolute simplicity of this clause of Catch-22 and let out a respectful whistle.|4 = }}&lt;br /&gt;
&lt;br /&gt;
Different formulations of &amp;quot;Catch-22&amp;quot; appear throughout the novel. The term is applied to various loopholes and quirks of the military system, always with the implication that rules are inaccessible to and slanted against those lower in the hierarchy. In chapter 6, Yossarian is told that Catch-22 requires him to do anything his [[commanding officer]] tells him to do, regardless of whether these orders contradict orders from the officer&#039;s superiors.&amp;lt;ref name=Henriksen&amp;gt;Margot A. Henriksen, &#039;&#039;Dr. Strangelove&#039;s America: Society and Culture in the Atomic Age&#039;&#039;; University of California Press, 1997; ISBN 0-520-08310-5; p. [http://books.google.com/books?id=KGrsQOIQgeYC&amp;amp;lpg=PP1&amp;amp;pg=PA250#v=onepage&amp;amp;q&amp;amp;f=false 250].&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
In a final episode, Catch-22 is described to Yossarian by an old woman recounting an act of violence by soldiers:&amp;lt;ref&amp;gt;&amp;quot;[http://www.answers.com/topic/joseph-heller Joseph Heller]&amp;quot;, &#039;&#039;Gale Encyclopedia of Biography&#039;&#039;, accessed via Answers.com, 16 August 2013.&amp;lt;/ref&amp;gt;&amp;lt;ref name=CombsNimmo /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
{{quotation|&amp;quot;Catch-22 says they have a right to do anything we can&#039;t stop them from doing.&amp;quot; &amp;lt;p&amp;gt; &amp;quot;What the hell are you talking about?&amp;quot; Yossarian shouted at her in bewildered, furious protest. &amp;quot;How did you know it was Catch-22? Who the hell told you it was Catch-22?&amp;quot; &amp;lt;p&amp;gt; &amp;quot;The soldiers with the hard white hats and clubs. The girls were crying. &#039;Did we do anything wrong?&#039; they said. The men said no and pushed them away out the door with the ends of their clubs. &#039;Then why are you chasing us out?&#039; the girls said. &#039;Catch 22,&#039; the men said. All they kept saying was &#039;Catch-22, Catch-22. What does it mean, Catch 22? What is Catch-22?&amp;quot; &amp;lt;p&amp;gt; &amp;quot;Didn&#039;t they show it to you?&amp;quot; Yossarian demanded, stamping about in anger and distress. &amp;quot;Didn&#039;t you even make them read it?&amp;quot; &amp;lt;p&amp;gt; &amp;quot;They don&#039;t have to show us Catch-22,&amp;quot; the old woman answered. &amp;quot;The law says they don&#039;t have to.&amp;quot; &amp;lt;p&amp;gt; &amp;quot;What law says they don&#039;t have to?&amp;quot; &amp;lt;p&amp;gt; &amp;quot;Catch-22&amp;quot;.}}&lt;br /&gt;
&lt;br /&gt;
According to literature professor Ian Gregson, the old woman&#039;s narrative defines &amp;quot;Catch-22&amp;quot; more directly as the &amp;quot;brutal operation of power&amp;quot;, stripping away the &amp;quot;bogus sophistication&amp;quot; of the earlier scenarios.&amp;lt;ref&amp;gt;Ian Gregson, &#039;&#039;Character and Satire in Post War Fiction&#039;&#039;; London: Continuum, 2006; ISBN 9781441130006; p. [http://books.google.com/books?id=e0qqaRTVt_sC&amp;amp;lpg=PP1&amp;amp;pg=PA38#v=onepage&amp;amp;q&amp;amp;f=false 38].&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
=== Other appearances in the novel ===&lt;br /&gt;
Besides referring to an unsolvable logical [[dilemma]], Catch-22 is invoked to explain or justify the military bureaucracy. For example, in the first chapter it requires Yossarian to sign his name to letters that he censors while he is confined to a hospital bed. One clause mentioned in chapter 10 closes a loophole in promotions, which one private had been exploiting to reattain the attractive rank of [[Private First Class]] after any promotion. Through [[courts-martial]] for going [[AWOL]], he would be busted in rank back to private, but Catch-22 limited the number of times he could do this before being sent to the stockade.&lt;br /&gt;
&lt;br /&gt;
At another point in the book, a prostitute explains to Yossarian that she cannot marry him because he is crazy, and she will never marry a crazy man. She considers any man crazy who would marry a woman who is not a virgin. This closed logic loop clearly illustrated Catch-22 because by her logic, all men who refuse to marry her are sane and thus she would consider marriage; but as soon as a man agrees to marry her, he becomes crazy for wanting to marry a non-virgin, and is instantly rejected.&lt;br /&gt;
&lt;br /&gt;
At one point, Captain Black attempts to pressure Milo into depriving Major Major of food as a consequence of not signing a loyalty oath that Major Major was never given an opportunity to sign in the first place. Captain Black asks Milo, &amp;quot;You&#039;re not against Catch-22, are you?&amp;quot; &lt;br /&gt;
&lt;br /&gt;
In chapter 40, Catch-22 forces Colonels Korn and Cathcart to promote Yossarian to Major and ground him rather than simply sending him home. They fear that if they do not, others will refuse to fly, just as Yossarian did.&lt;br /&gt;
&lt;br /&gt;
=== Significance of the number 22 ===&lt;br /&gt;
{{main|Catch-22#Explanation of the novel&#039;s title|Catch-22}}&lt;br /&gt;
Heller originally wanted to call the phrase, and hence the book, by other numbers, but he and his publishers eventually settled on 22. The number has no particular significance; it was chosen more or less for [[euphony]]. The title was originally &#039;&#039;Catch-18&#039;&#039;, but Heller changed it after the popular &#039;&#039;[[Mila 18]]&#039;&#039; was published a short time beforehand.&amp;lt;ref name=&amp;quot;Aldridge1986&amp;quot; /&amp;gt;&amp;lt;ref name=Telegraph /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
== Usage ==&lt;br /&gt;
&lt;br /&gt;
The term &amp;quot;catch-22&amp;quot; has filtered into common usage in the English language.&amp;lt;ref name=OALD /&amp;gt; In a 1975 interview, Heller said the term would not translate well into other languages.&amp;lt;ref name=Telegraph&amp;gt;&amp;quot;[http://www.telegraph.co.uk/culture/3669372/A-classic-by-any-other-name.html A classic by any other name]&amp;quot;, &#039;&#039;The Telegraph&#039;&#039;, 18 November 2007.&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
James E. Combs and Dan D. Nimmo suggest that the idea of a &amp;quot;catch-22&amp;quot; has gained popular currency because so many people in modern society are exposed to frustrating bureaucratic logic. They write:&lt;br /&gt;
&lt;br /&gt;
&amp;lt;blockquote&amp;gt;Everyone, then, who deals with organizations understands the bureaucratic logic of Catch-22. In high school or college, for example, students can participate in student government, a form of self-government and democracy that allows them to decide whatever they want, just so long as the principal or dean of students approves. This bogus democracy that can be overruled by arbitrary fiat is perhaps a citizen&#039;s first encounter with organizations that may profess &#039;open&#039; and libertarian values, but in fact are closed and hierarchical systems. Catch-22 is an organizational assumption, an unwritten law of informal power that excepts the organization from responsibility and accountability, and puts the individual in the absurd position of being excepted for the convenience or unknown purposes of the organization. &amp;lt;ref name=CombsNimmo&amp;gt;James E. Combs &amp;amp; Dan D. Nimmo, &#039;&#039;The Comedy of Democracy&#039;&#039;; Westport, CT: Praeger (Greenwood Publishing Group), 1996; ISBN 0-275-94979-6; p. [http://books.google.com/books?id=VJw9OdBFgmgC&amp;amp;lpg=PP1&amp;amp;pg=PA152#v=onepage&amp;amp;q&amp;amp;f=false 152].&amp;lt;/ref&amp;gt;&amp;lt;/blockquote&amp;gt; &lt;br /&gt;
&lt;br /&gt;
Along with George Orwell&#039;s &amp;quot;[[doublethink]]&amp;quot;, &amp;quot;Catch-22&amp;quot; has become one of the best-recognized ways to describe the predicament of being trapped by contradictory rules.&amp;lt;ref&amp;gt;Richard King, &amp;quot;[http://thesmartset.com/article/article07181101.aspx 22 Going on 50: Half a century later, the world is full of Catch-22s]&amp;quot;; &#039;&#039;The Smart Set&#039;&#039;, 20 July 2011.&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
== Logic ==&lt;br /&gt;
&lt;br /&gt;
The [[Archetype|archetypal]] &#039;&#039;catch-22&#039;&#039;, as formulated by [[Joseph Heller|Heller]], involves the case of [[John Yossarian]], a [[United States Army Air Corps|U.S. Army Air Forces]] [[Bombardier (air force)|bombardier]], who wishes to be grounded from combat flight. This will only happen if he is evaluated by the squadron&#039;s [[flight surgeon]] and found &amp;quot;unfit to fly&amp;quot;. &amp;quot;Unfit&amp;quot; would be any pilot who is willing to fly such dangerous missions, as one would have to be [[Insanity|mad]] to volunteer for possible death. However, to be evaluated, he must &#039;&#039;request&#039;&#039; the evaluation, an act that is considered sufficient proof for being declared sane. These conditions make it impossible to be declared &amp;quot;unfit&amp;quot;.&lt;br /&gt;
&lt;br /&gt;
The &amp;quot;Catch-22&amp;quot; is that &amp;quot;anyone who wants to get out of combat duty isn&#039;t really crazy&amp;quot;.&amp;lt;ref name=&amp;quot;Heller1999&amp;quot; /&amp;gt; Hence, pilots who request a mental fitness evaluation &#039;&#039;are&#039;&#039; sane, and therefore must fly in combat. At the same time, if an evaluation is not requested by the pilot, he will never receive one and thus can never be found insane, meaning he must also fly in combat.&lt;br /&gt;
&lt;br /&gt;
Therefore, Catch-22 ensures that no pilot can ever be grounded for being insane even if he is.&lt;br /&gt;
&lt;br /&gt;
A logical formulation of this situation is:&lt;br /&gt;
&lt;br /&gt;
# &amp;lt;math&amp;gt;(E \rightarrow (I \land R))&amp;lt;/math&amp;gt; ([[Premise]]: If a person is excused from flying (E) because of mental illness, that must be because he is both insane (I), and requests an evaluation (R));&lt;br /&gt;
# &amp;lt;math&amp;gt;(I \rightarrow \neg R)&amp;lt;/math&amp;gt; ([[Premise]]: If a person is insane (I), he should not realize that he is, and would have no reason to request an evaluation)&lt;br /&gt;
# &amp;lt;math&amp;gt;(\neg I \or \neg R)&amp;lt;/math&amp;gt; (2, [[Material implication (rule of inference)|Definition of implication]]: since an insane person would not request an evaluation, it follows that all people must either not be insane, or not request an evaluation)&lt;br /&gt;
# &amp;lt;math&amp;gt;(\neg (I \land R))&amp;lt;/math&amp;gt; (3, [[De Morgan&#039;s laws|De Morgan]]: since all people must either not be insane, or not request an evaluation, it follows that no person is both insane and requests an evaluation)&lt;br /&gt;
# &amp;lt;math&amp;gt;(\neg E)&amp;lt;/math&amp;gt; (4, 1, [[Modus Tollens]]: since a person may be excused from flying only if he is both insane and requests an evaluation, but no person &#039;&#039;can&#039;&#039; be both insane and request an evaluation, it follows that no person can be excused from flying for reasons of insanity)&lt;br /&gt;
&lt;br /&gt;
Philosophy professor Laurence Goldstein argues that the &#039;airman&#039;s dilemma&#039; is logically not even a condition that is true under no circumstances; it is a &amp;quot;vacuous biconditional&amp;quot; that is ultimately meaningless. Goldstein writes:&amp;lt;ref&amp;gt;Laurence Goldstein, &amp;quot;[http://philpapers.org/rec/GOLTBR The Barber, Russell&#039;s paradox, catch-22, God, contradiction and more: A defence of a Wittgensteinian conception of contradiction]&amp;quot;; in &#039;&#039;The law of non-contradiction: new philosophical essays&#039;&#039;, ed. Graham Priest, Jc Beall &amp;amp; Bradley Armour-Garb; Oxford University Press, 2004.&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
{{quotation|The catch is this: what looks like a statement of the conditions under which an airman can be excused flying dangerous missions reduces not to the statement&lt;br /&gt;
&lt;br /&gt;
:(i) `An airman can be excused flying dangerous missions if and only if Cont’ (where `Cont’ is a contradiction)  &lt;br /&gt;
 &lt;br /&gt;
(which could be a mean way of disguising an unpleasant truth), but to the worthlessly empty announcement &lt;br /&gt;
 &lt;br /&gt;
:(ii) `An airman can be excused flying dangerous missions if and only if it is not the case that an airman can be excused flying dangerous missions’ &lt;br /&gt;
 &lt;br /&gt;
If the catch were (i), that would not be so bad – an airman would at least be able to discover that under no circumstances could he avoid combat duty. But Catch-22 is worse – a welter of words that amounts to nothing; it is without content, it conveys no information at all.}}&lt;br /&gt;
&lt;br /&gt;
== See also ==&lt;br /&gt;
{{portal|Novels}}&lt;br /&gt;
* [[Begging the question]]&lt;br /&gt;
* [[Cornelian dilemma]] &lt;br /&gt;
* [[Deadlock]]&lt;br /&gt;
* [[Double bind]]&lt;br /&gt;
* [[False dilemma]]&lt;br /&gt;
* [[Ironic process theory]]&lt;br /&gt;
* [[No-win situation]]&lt;br /&gt;
* [[List of paradoxes]]&lt;br /&gt;
* [[Mu_(negative)#.22Unasking.22_the_question|Mu]] &lt;br /&gt;
* [[Pyrrhic victory]]&lt;br /&gt;
* [[Social trap]]&lt;br /&gt;
* [[Vicious circle]]&lt;br /&gt;
&lt;br /&gt;
===Related stories and logic problems===&lt;br /&gt;
* [[Hobson&#039;s choice]] – Choice between taking what is offered and taking nothing; named after James Hobson, owner of a livery stable who required his customers to take the horse nearest the door&lt;br /&gt;
* [[Kobayashi Maru]] – A scenario involving a choice presented to a cadet in &#039;&#039;[[Star Trek]]&#039;&#039; where they either violate military regulations concerning the rendering of aid to a freighter crippled by a mine and in imminent threat of destruction, or violate the terms of a peace treaty by crossing into enemy territory (where the freighter lies in distress), risking one&#039;s company and crew to attempt to save the crippled freighter, and committing an act of war in the process of violating that treaty&lt;br /&gt;
* [[The Lady, or the Tiger?]] – A short story involving a princess who must make a decision in a no-win situation&lt;br /&gt;
* [[Morton&#039;s Fork]]&lt;br /&gt;
* [[Zugzwang]]&lt;br /&gt;
&lt;br /&gt;
== References ==&lt;br /&gt;
&lt;br /&gt;
{{reflist&lt;br /&gt;
| refs =&lt;br /&gt;
&lt;br /&gt;
&amp;lt;ref name=&amp;quot;Heller1999&amp;quot;&amp;gt;&lt;br /&gt;
{{cite book&lt;br /&gt;
| last = Heller&lt;br /&gt;
| first = Joseph&lt;br /&gt;
| authorlink = Joseph Heller&lt;br /&gt;
| title = Catch-22: A Novel&lt;br /&gt;
| page = 52&lt;br /&gt;
| publisher = Simon and Schuster&lt;br /&gt;
| year = 1999&lt;br /&gt;
| isbn = 978-0-684-86513-3&lt;br /&gt;
| url = http://books.google.com/books?id=Xfze51E7TEoC&amp;amp;lpg=PP1&amp;amp;dq=isbn%3A9780684865133&amp;amp;pg=PA52&lt;br /&gt;
| accessdate = 2011-01-09&lt;br /&gt;
}}&lt;br /&gt;
&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;ref name=&amp;quot;Aldridge1986&amp;quot;&amp;gt;&lt;br /&gt;
{{cite news&lt;br /&gt;
| last = Aldridge&lt;br /&gt;
| first = John W.&lt;br /&gt;
| authorlink = John W. Aldridge&lt;br /&gt;
| title = The Loony Horror of it All&amp;amp;nbsp;– &#039;Catch-22&#039; Turns 25&lt;br /&gt;
| newspaper = The New York Times&lt;br /&gt;
| date = 1986-10-26&lt;br /&gt;
| page = Section 7, Page 3, Column 1&lt;br /&gt;
| url = http://www.nytimes.com/books/98/02/15/home/heller-loony.html&lt;br /&gt;
| accessdate = 2011-01-09&lt;br /&gt;
}}&lt;br /&gt;
&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
}}&lt;br /&gt;
&lt;br /&gt;
{{DEFAULTSORT:Catch-22 (Logic)}}&lt;br /&gt;
[[Category:English idioms]]&lt;br /&gt;
[[Category:Paradoxes]]&lt;br /&gt;
[[Category:Catch-22]]&lt;br /&gt;
[[Category:Metaphors referring to war and violence]]&lt;br /&gt;
[[Category:Dilemmas]]&lt;br /&gt;
&lt;br /&gt;
[[ru:Уловка 22]]&lt;br /&gt;
[[sv:Moment 22]]&lt;/div&gt;</summary>
		<author><name>PenelopRosenste</name></author>
	</entry>
	<entry>
		<id>https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=49534</id>
		<title>Main Page</title>
		<link rel="alternate" type="text/html" href="https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=49534"/>
		<updated>2014-08-13T07:06:43Z</updated>

		<summary type="html">&lt;p&gt;PenelopRosenste: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{Refimprove|date=July 2009}}&lt;br /&gt;
&lt;br /&gt;
[[File:Lift-induced vortices behind aircraft (DLR demonstration).ogv|thumb|Lift-induced vortices behind a jet aircraft are evidenced by smoke on a runway]]&lt;br /&gt;
[[File:2011-06-05 19-32 Berlin TXL Airplane Flyover plus Wingtip Vortex.ogg|thumb|An audio recording of lift-induced vortices heard shortly after an airliner overfly]]&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;&#039;Wingtip vortices&#039;&#039;&#039; are circular patterns of rotating air left behind a [[wing]] as it generates [[Lift (force)|lift]].&amp;lt;ref name=Clancy5.14&amp;gt;Clancy, L.J., &#039;&#039;Aerodynamics&#039;&#039;, section 5.14&amp;lt;/ref&amp;gt;  One wingtip [[vortex]] trails from the [[Wing tip|tip]] of each wing.  Wingtip vortices are sometimes named &#039;&#039;trailing&#039;&#039; or &#039;&#039;lift-induced vortices&#039;&#039; because they also occur at points other than at the wing tips.&amp;lt;ref name=Clancy5.14/&amp;gt; Indeed, vorticity is trailed at any point on the wing where the lift varies span-wise (a fact described and quantified by the [[lifting-line theory]]); it eventually rolls up into large vortices near the wingtip, at the edge of [[Flap (aircraft)|flap devices]], or at other abrupt changes in [[planform|wing planform]].&lt;br /&gt;
&lt;br /&gt;
Wingtip vortices are associated with [[induced drag]], the imparting of [[downwash]], and are a fundamental consequence of three-dimensional lift generation.&amp;lt;ref&amp;gt;Clancy, L.J., &#039;&#039;Aerodynamics&#039;&#039;, sections 5.17 and 8.9&amp;lt;/ref&amp;gt;  Careful selection of wing geometry (in particular, [[Aspect ratio (wing)|aspect ratio]]), as well as of cruise conditions, are design and operational methods to minimize induced drag.&lt;br /&gt;
&lt;br /&gt;
Wingtip vortices form the primary component of [[wake turbulence]]. Depending on ambient atmospheric humidity as well as the geometry and wing loading of aircraft, water may condense or freeze in the core of the vortices, making the vortices visible.&lt;br /&gt;
&lt;br /&gt;
== Generation of trailing vortices ==&lt;br /&gt;
[[Image:Tip vortex rollup.png|thumb|Euler computation of a tip vortex rolling up from the trailed vorticity sheet.]]&lt;br /&gt;
When a wing generates [[lift (force)|aerodynamic lift]] the air on the top surface has lower pressure relative to the bottom surface. Air flows from below the wing and out around the tip to the top of the wing in a circular fashion. An emergent circulatory flow pattern named [[vortex]] is observed, featuring a low-pressure core.&lt;br /&gt;
&lt;br /&gt;
Three-dimensional lift and the occurrence of wingtip vortices can be approached with the concept of [[horseshoe vortex]] and described accurately with the [[Lifting-line theory|Lanchester–Prandtl theory]]. In this view, the trailing vortex is a continuation of the &#039;&#039;wing-bound vortex&#039;&#039; inherent to the lift generation.&lt;br /&gt;
&lt;br /&gt;
If viewed from the tail of the airplane, looking forward in the direction of flight, there is one wingtip vortex trailing from the left-hand wing and circulating clockwise, and another one trailing from the right-hand wing and circulating anti-clockwise. The result is a region of downwash behind the aircraft, between the two vortices.&lt;br /&gt;
&lt;br /&gt;
The two wingtip vortices do not merge because they are circulating in opposite directions. They dissipate slowly and linger in the atmosphere long after the airplane has passed. They are a hazard to other aircraft, known as [[wake turbulence]].&lt;br /&gt;
&lt;br /&gt;
== Effects and mitigation ==&lt;br /&gt;
&lt;br /&gt;
[[File:Air France Boeing 777-300ER planform view.jpg|thumb|Modern airliners often feature [[Aspect ratio (wing)|slender wings]] and [[wingtip device]]s]]&lt;br /&gt;
&lt;br /&gt;
Wingtip vortices are associated with [[induced drag]], an unavoidable consequence of three-dimensional lift generation. The rotary motion of the air within the shed wingtip vortices (sometimes described as a &amp;quot;leakage&amp;quot;) reduces the effective [[angle of attack]] of the air on the wing.&lt;br /&gt;
&lt;br /&gt;
The [[lifting-line theory]] describes the shedding of trailing vortices as span-wise changes in lift distribution. For a given wing span and surface, minimal induced drag is obtained with an [[Elliptical wing|elliptical lift distribution]]. For a given lift distribution and surface, induced drag is reduced with increasing [[Aspect ratio (wing)|aspect ratio]].&lt;br /&gt;
&lt;br /&gt;
As a consequence, aircraft for which a high [[lift-to-drag ratio]] is desirable, such as [[Glider aircraft|gliders]] or long-range [[airliner]]s, typically have high aspect ratio wings. Such wings however have disadvantages with respect to structural constraints and manoeuvrability, as evidenced by [[Fighter aircraft|combat]] and [[Aerobatics|aerobatic]] planes which usually feature short, stubby wings despite the efficiency losses.&lt;br /&gt;
&lt;br /&gt;
Another method of reducing induced drag is the use of [[Wingtip device|winglets]], as seen on most modern airliners. Winglets increase the effective aspect ratio of the wing, changing the pattern and magnitude of the [[vorticity]] in the vortex pattern. A reduction is achieved in the kinetic energy in the circular air flow, which reduces the amount of fuel expended to perform work upon the spinning air.&lt;br /&gt;
&lt;br /&gt;
== Visibility of vortices ==&lt;br /&gt;
&lt;br /&gt;
[[File:FA-18C vapor LEX and wingtip 1.jpg|thumb|Vortices shed at the tips and from the [[leading-edge extension]]s of an F/A-18]]&lt;br /&gt;
&lt;br /&gt;
The cores of the vortices are sometimes visible because water present in them [[condensation|condenses]] from [[gas]] ([[vapor]]) to [[liquid]], and sometimes even freezes, forming ice particles.&lt;br /&gt;
&lt;br /&gt;
Condensation of water vapor in wing tip vortices is most common on aircraft flying at high [[angle of attack|angles of attack]], such as fighter aircraft in high [[g-force|&#039;&#039;g&#039;&#039;]] maneuvers, or [[airliner]]s taking off and landing on humid days.&lt;br /&gt;
&lt;br /&gt;
=== Aerodynamic condensation and freezing ===&lt;br /&gt;
{{Anchor|Discussion of the physics of aerodynamic condensation and freezing}}&lt;br /&gt;
&lt;br /&gt;
The cores of vortices spin at very high speed and are regions of very low pressure. To [[Orders of approximation|first approximation]], these low-pressure regions form with little exchange of heat with the neighboring regions (i.e., [[Adiabatic process|adiabatically]]), so the local temperature in the low-pressure regions drops, too.&amp;lt;ref name=&amp;quot;Green Fluid Vortices&amp;quot;&amp;gt;Green, S. I. [http://books.google.com/books?id=j6qE7YAwwCoC&amp;amp;pg=PA427&amp;amp;lpg=PA427&amp;amp;dq=condensation+in+wingtip+vortices&amp;amp;source=bl&amp;amp;ots=S8a5ApDgog&amp;amp;sig=wMqbujbSVVVVGJ9yNq9CnQyW368&amp;amp;hl=en&amp;amp;ei=E6BLSpj2FZqytwfT0PibDQ&amp;amp;sa=X&amp;amp;oi=book_result&amp;amp;ct=result&amp;amp;resnum=8 “Wing tip vortices”] in &#039;&#039;Fuid vortices,&#039;&#039; S. I. Green, ed. ([[Kluwer]], Amsterdam, 1995) pp. 427-470. ISBN 978-0-7923-3376-0&amp;lt;/ref&amp;gt;  If it drops below the local [[dew point]], there results a condensation of water vapor present in the cores of wingtip vortices, making them visible.&amp;lt;ref name=&amp;quot;Green Fluid Vortices&amp;quot;/&amp;gt; The temperature may even drop below the local [[freezing point]], in which case ice crystals will form inside the cores.&amp;lt;ref name=&amp;quot;Green Fluid Vortices&amp;quot; /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
The [[Phase (matter)|phase]] of water (i.e., whether it assumes the form of a solid, liquid, or gas) is determined by its [[temperature]] and [[pressure]]. For example, in the case of liquid-gas transition, at each pressure there is a special “transition temperature” &amp;lt;math&amp;gt;T_{c}&amp;lt;/math&amp;gt; such that if the sample temperature is even a little above &amp;lt;math&amp;gt;T_{c}&amp;lt;/math&amp;gt;, the sample will be a gas, but, if the sample temperature is even a little below &amp;lt;math&amp;gt;T_{c}&amp;lt;/math&amp;gt;, the sample will be a liquid; see [[phase transition]]. For example, at the [[standard conditions|standard atmospheric pressure]], &amp;lt;math&amp;gt;T_{c}&amp;lt;/math&amp;gt; is 100&amp;amp;nbsp;°C&amp;amp;nbsp;=&amp;amp;nbsp;212&amp;amp;nbsp;°F. The transition temperature &amp;lt;math&amp;gt;T_{c}&amp;lt;/math&amp;gt; decreases with decreasing pressure (which explains why water boils at lower temperatures at higher altitudes and at higher temperatures in a [[pressure cooker]]; see [[Vapor pressure#Water vapor pressure|here]] for more information). In the case of water vapor in air, the &amp;lt;math&amp;gt;T_{c}&amp;lt;/math&amp;gt; corresponding to the [[partial pressure]] of water vapor is called the [[dew point]]. (The solid–liquid transition also happens around a specific transition temperature called the [[melting point]]. For most substances, the melting point also decreases with decreasing pressure, although water ice in particular - in its [[Ice Ih|I&amp;lt;sub&amp;gt;h&amp;lt;/sub&amp;gt; form]], which is [[Phases of ice|the most familiar one]] - is a prominent [[Water (properties)|exception to this rule]].)&lt;br /&gt;
&lt;br /&gt;
Vortex cores are regions of low pressure. As a vortex core begins to form, the water in the air (in the region that is about to become the core) is in vapor phase, which means that the local temperature is above the local dew point. After the vortex core forms, the pressure inside it has decreased from the ambient value, and so the local dew point (&amp;lt;math&amp;gt;T_{c}&amp;lt;/math&amp;gt;) has dropped from the ambient value. Thus, &#039;&#039;in and of itself&#039;&#039;, a drop in pressure would tend to keep water in vapor form: The initial dew point was already below the ambient air temperature, and the formation of the vortex has made the local dew point even lower. However, as the vortex core forms, its pressure (and so its dew point) is not the only property that is dropping: The vortex-core temperature is dropping also, and in fact it can drop by much more than the dew point does, as we now explain.&lt;br /&gt;
&lt;br /&gt;
Here we follow the discussion in Ref.&amp;lt;ref name=&amp;quot;Green Fluid Vortices&amp;quot; /&amp;gt; To [[Orders of approximation|first approximation]], the formation of vortex cores is [[thermodynamics|thermodynamically]] an [[adiabatic process]], i.e., one with no exchange of heat. In such a process, the drop in pressure is accompanied by a drop in temperature, according to the equation&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;\frac{T_{\text{f}}}{T_{\text{i}}}=\left(\frac{p_{\text{f}}}{p_{\text{i}}}\right)^{\frac{\gamma -1}{\gamma}}.&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Here &amp;lt;math&amp;gt;T_{\text{i}}&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;p_{\text{i}}&amp;lt;/math&amp;gt; are the [[Thermodynamic temperature|absolute temperature]] and pressure at the beginning of the process (here equal to the ambient air temperature and pressure), &amp;lt;math&amp;gt;T_{\text{f}}&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;p_{\text{f}}&amp;lt;/math&amp;gt; are the absolute temperature and pressure in the vortex core (which is the end result of the process), and the constant &amp;lt;math&amp;gt;\gamma&amp;lt;/math&amp;gt; is about 7/5&amp;amp;nbsp;=&amp;amp;nbsp;1.4 for air (see [[Adiabatic process#Ideal gas (reversible case only)|here]]).&lt;br /&gt;
&lt;br /&gt;
Thus, even though the local dew point inside the vortex cores is even lower than in the ambient air, the water vapor may nevertheless condense — if the formation of the vortex brings the local temperature below the new local dew point. Let&#039;s verify that this can indeed happen under realistic conditions.&lt;br /&gt;
&lt;br /&gt;
For a typical transport aircraft landing at an airport, these conditions are as follows: We may take &amp;lt;math&amp;gt;T_{\text{i}}&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;p_{\text{i}}&amp;lt;/math&amp;gt; to have values corresponding to the so-called [[standard conditions]], i.e., &amp;lt;math&amp;gt;p_{\text{i}}&amp;lt;/math&amp;gt;&amp;amp;nbsp;=&amp;amp;nbsp;1&amp;amp;nbsp;[[Atmosphere (unit)|atm]]&amp;amp;nbsp;=&amp;amp;nbsp;1013.25&amp;amp;nbsp;[[Bar (unit)|mb]]&amp;amp;nbsp;=&amp;amp;nbsp;101&amp;lt;math&amp;gt;\,&amp;lt;/math&amp;gt;325&amp;amp;nbsp;[[Pascal (unit)|Pa]] and &amp;lt;math&amp;gt;T_{\text{i}}&amp;lt;/math&amp;gt;&amp;amp;nbsp;=&amp;amp;nbsp;293.15&amp;amp;nbsp;[[Kelvin (unit)|K]] (which is 20&amp;amp;nbsp;°C&amp;amp;nbsp;=&amp;amp;nbsp;68&amp;amp;nbsp;°F). We will take the [[relative humidity]] to be a [[dew point#Human reaction to high dew points|comfortable]] 35% (dew point of 4.1&amp;amp;nbsp;°C&amp;amp;nbsp;=&amp;amp;nbsp;39.4&amp;amp;nbsp;°F). This corresponds to a [[partial pressure]] of water vapor of 820&amp;amp;nbsp;Pa&amp;amp;nbsp;=&amp;amp;nbsp;8.2&amp;amp;nbsp;mb. We will assume that in a vortex core, the pressure (&amp;lt;math&amp;gt;p_{\text{f}}&amp;lt;/math&amp;gt;) drops to about 80% of the ambient pressure, i.e., to about 80&amp;amp;nbsp;000&amp;amp;nbsp;Pa.&amp;lt;ref name=&amp;quot;Green Fluid Vortices&amp;quot; /&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Let&#039;s &amp;lt;!--&amp;quot;Let us&amp;quot; does not mean &amp;quot;let&#039;s.&amp;quot;--&amp;gt;first determine the temperature in the vortex core. It is given by the equation above as &amp;lt;math&amp;gt;T_{\text{f}}=\left(\frac{\scriptstyle 80\,000}{\scriptstyle 101\,325}\right)^{\scriptscriptstyle 0.4/1.4}\,T_{\text{i}}= 0.935\,\times\,293.15=274\;\text{K},&amp;lt;/math&amp;gt; or 0.86&amp;amp;nbsp;°C&amp;amp;nbsp;=&amp;amp;nbsp;33.5&amp;amp;nbsp;°F.&lt;br /&gt;
&lt;br /&gt;
Next, we determine the dew point in the vortex core. The partial pressure of water in the vortex core drops in proportion to the drop in the total pressure (i.e., by the same percentage), to about 650&amp;amp;nbsp;Pa&amp;amp;nbsp;=&amp;amp;nbsp;6.5&amp;amp;nbsp;mb. According to a dew point calculator at [http://antoine.frostburg.edu/chem/senese/javascript/water-properties.html this site] (as an alternative, one may use the [[Antoine equation]] to obtain an approximate value), that partial pressure results in the local dew point of about 0.86&amp;amp;nbsp;°C; in other words, the new local dew point is about equal to the new local temperature.&lt;br /&gt;
&lt;br /&gt;
Therefore, the case we have been considering is a marginal case; if the relative humidity of the ambient air were even a bit higher (with the total pressure and temperature remaining as above), then the local dew point inside the vortices would rise, while the local temperature would remain the same as what we have just found. Thus, the local temperature would now be &#039;&#039;lower&#039;&#039; than the local dew point, and so the water vapor inside the vortices would indeed condense. Under right conditions, the local temperature in vortex cores may drop below the local [[freezing point]], in which case ice particles will form inside the vortex cores.&lt;br /&gt;
&lt;br /&gt;
We have just seen that the water-vapor condensation mechanism in wingtip vortices is driven by local changes in air pressure and temperature. This is to be contrasted to what happens in another well-known case of water condensation related to airplanes: the [[contrail]]s from airplane engine exhausts. In the case of contrails, the local air pressure and temperature do not change significantly; what matters instead is that the exhaust contains both water vapor (which increases the local water-vapor [[concentration]] and so its partial pressure, resulting in elevated dew point and freezing point) as well as [[aerosol]]s (which provide [[Nucleation|nucleation centers]] for the [[Condensation (aerosol dynamics)|condensation]] and freezing).&amp;lt;ref&amp;gt;[http://asd-www.larc.nasa.gov/GLOBE/science.html NASA, Contrail Science]{{dead link|date=May 2014}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
== Formation flight ==&lt;br /&gt;
[[File:CanadianGeeseFlyingInVFormation.jpg|thumb|[[Canada goose|Canada geese]] in [[V formation]] make use of each bird&#039;s wingtip vortices]]&lt;br /&gt;
&lt;br /&gt;
Migratory birds take advantage of each other&#039;s wingtip vortices by flying in a [[V formation]] so that all but the leader are flying in the [[downwash|upwash]] from the wing of the bird ahead. This upwash makes it easier for the bird to support its own weight, reducing fatigue on migration flights.&amp;lt;ref&amp;gt;{{cite conference |author=Thien, H.P. |author2=Moelyadi, M.A |author3=Muhammad, H.  |url=http://arxiv.org/abs/0804.3879 |title=Effects of Leader’s Position and Shape on Aerodynamic Performances of V Flight Formation, Paper No. ICIUS2007-A008 |booktitle=Proceedings of the International Conference on Intelligent Unmanned System (ICIUS 2007) | pages=1–7| date=October 24–25, 2007 |location=Bali, Indonesia |publisher=Aeronautics and Astronautics Department Bandung Institute of Technology (via Arxiv.org) |accessdate=29 May 2014}} &amp;lt;br/&amp;gt;([http://arxiv.org/pdf/0804.3879v1 Download paper]. {{PDF|336 Kb}})&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
== Hazards ==&lt;br /&gt;
[[Image:Airplane vortex edit.jpg|thumb|right|A [[NASA]] study on wingtip vortices produced illustrating the size of the vortices produced.]]&lt;br /&gt;
&lt;br /&gt;
Wingtip vortices can pose a hazard to aircraft, especially during the [[landing]] and [[takeoff]] phases of flight. The intensity or strength of the vortex is a function of aircraft size, speed, and configuration (flap setting, etc.). The strongest vortices are produced by heavy aircraft, flying slowly, {{Citation needed span|text=with [[Flap (aircraft)|wing flaps]] and landing gear retracted (&amp;quot;heavy, slow, and clean&amp;quot;)|date=July 2012}}.  Large [[jet aircraft]] can generate vortices that can persist for many minutes, drifting with the wind.&lt;br /&gt;
&lt;br /&gt;
The hazardous aspects of wingtip vortices are most often discussed in the context of [[wake turbulence]].  If a light aircraft is immediately preceded by a heavy aircraft, wake turbulence from the heavy aircraft can roll the light aircraft faster than can be resisted by use of ailerons. At low altitudes, in particular during takeoff and landing, this can lead to an upset from which recovery is not possible.  [[Air traffic controller]]s attempt to ensure an adequate separation between departing and arriving aircraft by issuing wake turbulence warnings to pilots.&lt;br /&gt;
&lt;br /&gt;
== Gallery ==&lt;br /&gt;
&amp;lt;gallery&amp;gt;&lt;br /&gt;
Image:EA-6B Prowler from VAQ-138.jpg|An [[EA-6 Prowler]] with condensation in the cores of its wingtip vortices and also on the top of its wings.&lt;br /&gt;
Image:Wingtip condensation.jpg|The core of the vortex trailing from the tip of the [[Flap (aircraft)|flap]] of a commercial airplane with landing flap extended.&lt;br /&gt;
Image:Cessna 182 model-wingtip-vortex.jpg|Wingtip vortices from a Cessna 182 [[wind tunnel]] model.&lt;br /&gt;
Image:C17-Vortex.JPG|Wingtip vortices shown in [[Flare (countermeasure)|flare]] smoke left behind a [[C-17 Globemaster III]].  Also known as smoke angels.&lt;br /&gt;
file:DN-SD-06-03008.JPG|The [[MV-22 Osprey]] [[tiltrotor]] has a high [[disk loading]], producing visible blade tip vorticies.&lt;br /&gt;
File:Euler tip vortex.png|Euler computation of a steady tip vortex. Contour colours and isosurface reveal vorticity.&lt;br /&gt;
File:Model in Vortex Facility - GPN-2000-001288.jpg|A [[Boeing 747]] model has just passed through a stationary sheet of smoke, which is showing its trailing vortices, at the Vortex Facility at the [[Langley Research Center]].&lt;br /&gt;
&amp;lt;/gallery&amp;gt;&lt;br /&gt;
&lt;br /&gt;
== See also ==&lt;br /&gt;
* [[Aspect ratio (wing)]]&lt;br /&gt;
* [[Contrail]]&lt;br /&gt;
* [[Helmholtz&#039;s theorems]]&lt;br /&gt;
* [[Horseshoe vortex]]&lt;br /&gt;
* [[Lift-induced drag]]&lt;br /&gt;
* [[V formation]]&lt;br /&gt;
* [[Vortex]]&lt;br /&gt;
* [[Wake turbulence]]&lt;br /&gt;
&lt;br /&gt;
==References==&lt;br /&gt;
*Clancy, L.J. (1975), &#039;&#039;Aerodynamics&#039;&#039;, Pitman Publishing Limited, London ISBN 0-273-01120-0&lt;br /&gt;
&lt;br /&gt;
===Notes===&lt;br /&gt;
{{reflist}}&lt;br /&gt;
&lt;br /&gt;
==External links==&lt;br /&gt;
{{Commons|Wingtip vortices}}&lt;br /&gt;
*Video from [[NASA]]&#039;s [[Dryden Flight Research Center]] tests on wingtip vortices:&lt;br /&gt;
**[[C-5 Galaxy]]: [http://www1.dfrc.nasa.gov/Gallery/Movie/C-5A/HTML/EM-0085-01.html]&lt;br /&gt;
**[[Lockheed L-1011]]: [http://www1.dfrc.nasa.gov/Gallery/Movie/L-1011/index.html]&lt;br /&gt;
*[http://www.ll.mit.edu/AviationWeather/WW-11077_WindPrediction.pdf Wind prediction for analysis of vortex drift]&lt;br /&gt;
*[http://antwrp.gsfc.nasa.gov/apod/ap060822.html Flares released by an air force jet form a &amp;quot;smoke angel&amp;quot;]&lt;br /&gt;
*[http://www.youtube.com/watch?v=PpUftG_mxg8 Wingtip Vortices during a landing - Video at Youtube]&lt;br /&gt;
&lt;br /&gt;
{{Aviation lists}}&lt;br /&gt;
&lt;br /&gt;
{{DEFAULTSORT:Wingtip Vortices}}&lt;br /&gt;
[[Category:Aviation risks]]&lt;br /&gt;
[[Category:Aerodynamics]]&lt;br /&gt;
[[Category:Vortices]]&lt;br /&gt;
[[Category:Aircraft wing design]]&lt;br /&gt;
&lt;br /&gt;
[[ja:ウェーク・タービュランス]]&lt;/div&gt;</summary>
		<author><name>PenelopRosenste</name></author>
	</entry>
	<entry>
		<id>https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=49530</id>
		<title>Main Page</title>
		<link rel="alternate" type="text/html" href="https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=49530"/>
		<updated>2014-08-13T07:05:25Z</updated>

		<summary type="html">&lt;p&gt;PenelopRosenste: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{Infobox Polyhedron with net |&lt;br /&gt;
  Image_File=Bilunabirotunda.png|&lt;br /&gt;
  Polyhedron_Type=[[Johnson solid|Johnson]]&amp;lt;br&amp;gt;[[disphenocingulum|J&amp;lt;sub&amp;gt;90&amp;lt;/sub&amp;gt;]] - &#039;&#039;&#039;J&amp;lt;sub&amp;gt;91&amp;lt;/sub&amp;gt;&#039;&#039;&#039; - [[triangular hebesphenorotunda|J&amp;lt;sub&amp;gt;92&amp;lt;/sub&amp;gt;]]|&lt;br /&gt;
  Face_List=2x4 [[triangle]]s&amp;lt;br&amp;gt;2 [[Square (geometry)|square]]s&amp;lt;br&amp;gt;4 [[pentagon]]s|&lt;br /&gt;
  Edge_Count=26|&lt;br /&gt;
  Vertex_Count=14|&lt;br /&gt;
  Symmetry_Group=&#039;&#039;D&#039;&#039;&amp;lt;sub&amp;gt;2h&amp;lt;/sub&amp;gt;||&lt;br /&gt;
  Vertex_List=4(3.5&amp;lt;sup&amp;gt;2&amp;lt;/sup&amp;gt;) &amp;lt;br&amp;gt; 8(3.4.3.5) &amp;lt;br&amp;gt; 2(3.5.3.5)|&lt;br /&gt;
  Dual=-|&lt;br /&gt;
  Property_List=[[Convex set|convex]]|&lt;br /&gt;
  Net_Image_File=Johnson solid 91 net.png&lt;br /&gt;
}}&lt;br /&gt;
&lt;br /&gt;
In [[geometry]], the &#039;&#039;&#039;bilunabirotunda&#039;&#039;&#039; is one of the [[Johnson solid]]s (&#039;&#039;J&#039;&#039;&amp;lt;sub&amp;gt;91&amp;lt;/sub&amp;gt;). It is one of the elementary Johnson solids that do not arise from &amp;quot;cut and paste&amp;quot; manipulations of the [[Platonic solid|Platonic]] and [[Archimedean solid|Archimedean]] solids.&lt;br /&gt;
&lt;br /&gt;
The 92 Johnson solids were named and described by [[Norman Johnson (mathematician)|Norman Johnson]] in 1966.&lt;br /&gt;
&lt;br /&gt;
== Cartesian coordinates ==&lt;br /&gt;
&amp;lt;p&amp;gt;The following define the vertices of a bilunabirotunda centered at the origin with edge length 1: &amp;lt;/p&amp;gt;&lt;br /&gt;
&amp;lt;dl&amp;gt;&lt;br /&gt;
&amp;lt;dd&amp;gt;&amp;lt;math&amp;gt;\left(0, 0, \pm\frac{\varphi}{2}\right)&amp;lt;/math&amp;gt;&amp;lt;/dd&amp;gt;&lt;br /&gt;
&amp;lt;dd&amp;gt;&amp;lt;math&amp;gt;\left(\pm\frac{(\varphi+1)}{2}, \pm\frac{1}{2}, 0\right)&amp;lt;/math&amp;gt;&amp;lt;/dd&amp;gt;&lt;br /&gt;
&amp;lt;dd&amp;gt;&amp;lt;math&amp;gt;\left(\pm\frac{1}{2},\pm\frac{\varphi}{2},\pm\frac{1}{2}\right)&amp;lt;/math&amp;gt;&amp;lt;/dd&amp;gt;&lt;br /&gt;
&amp;lt;/dl&amp;gt;&lt;br /&gt;
&amp;lt;p&amp;gt;where &amp;lt;math&amp;gt;\varphi=\frac{1+\sqrt{5}}{2} &amp;lt;/math&amp;gt; is the golden ratio.&amp;lt;/p&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==External links==&lt;br /&gt;
* {{MathWorld | urlname=JohnsonSolid | title=Johnson Solid}}&lt;br /&gt;
** {{MathWorld | urlname=Bilunabirotunda | title=Bilunabirotunda}}&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
{{Polyhedron-stub}}&lt;br /&gt;
[[Category:Johnson solids]]&lt;br /&gt;
&lt;br /&gt;
[[es:Bilunabirrotonda]]&lt;br /&gt;
[[eo:J91]]&lt;br /&gt;
[[fr:Birotonde bilunaire]]&lt;br /&gt;
[[it:Bilunabirotunda]]&lt;br /&gt;
[[nl:Bilunabirotonde]]&lt;br /&gt;
[[zh:雙新月雙罩帳]]&lt;/div&gt;</summary>
		<author><name>PenelopRosenste</name></author>
	</entry>
	<entry>
		<id>https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=48367</id>
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		<link rel="alternate" type="text/html" href="https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=48367"/>
		<updated>2014-08-13T00:59:59Z</updated>

		<summary type="html">&lt;p&gt;PenelopRosenste: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{Unreferenced|date=August 2009}}&lt;br /&gt;
[[File:OrbitalEccentricityDemo.svg|thumb|right|The green path in this image is an example of a parabolic trajectory.]]&lt;br /&gt;
[[File:Gravity Wells Potential Plus Kinetic Energy - Circle-Ellipse-Parabola-Hyperbola.png|thumb|250px|A parabolic trajectory is depicted in the bottom-left quadrant of this diagram, where the [[gravity well|gravitational potential well]] of the central mass shows potential energy, and the kinetic energy of the parabolic trajectory is shown in red. The height of the kinetic energy decreases asymptotically toward zero as the speed decreases and distance increases according to Kepler&#039;s laws.]]&lt;br /&gt;
{{about|a class of Kepler orbits|a free body trajectory at constant gravity|Ballistic trajectory}}&lt;br /&gt;
In [[astrodynamics]] or [[celestial mechanics]] a &#039;&#039;&#039;parabolic trajectory&#039;&#039;&#039; is a [[Kepler orbit]] with the [[Orbital eccentricity|eccentricity]] equal to 1. When moving away from the source it is called an &#039;&#039;&#039;escape orbit&#039;&#039;&#039;, otherwise a &#039;&#039;&#039;capture orbit&#039;&#039;&#039;. It is also sometimes referred to as a &#039;&#039;&#039;C&amp;lt;sub&amp;gt;3&amp;lt;/sub&amp;gt;&amp;amp;nbsp;=&amp;amp;nbsp;0 orbit&#039;&#039;&#039;.&lt;br /&gt;
&lt;br /&gt;
Under standard assumptions a body traveling along an escape orbit will [[orbital coast|coast]] along a [[Parabola|parabolic]] shaped trajectory to infinity, with velocity relative to the [[central body]] tending to zero, and therefore will never return. Parabolic trajectory are minimum-energy escape trajectories, separating positive-[[characteristic energy|energy]] [[hyperbolic trajectory|hyperbolic trajectories]] from negative-energy [[elliptic orbit]]s.&lt;br /&gt;
&lt;br /&gt;
==Velocity==&lt;br /&gt;
Under standard assumptions the [[orbital velocity]] (&amp;lt;math&amp;gt;v\,&amp;lt;/math&amp;gt;) of a body travelling along parabolic trajectory can be computed as:&lt;br /&gt;
:&amp;lt;math&amp;gt;v=\sqrt{2\mu\over{r}}&amp;lt;/math&amp;gt;&lt;br /&gt;
where:&lt;br /&gt;
*&amp;lt;math&amp;gt;r\,&amp;lt;/math&amp;gt; is the radial distance of orbiting body from [[central body]],&lt;br /&gt;
*&amp;lt;math&amp;gt;\mu\,&amp;lt;/math&amp;gt; is the [[standard gravitational parameter]].&lt;br /&gt;
&lt;br /&gt;
At any position the orbiting body has the [[escape velocity]] for that position.&lt;br /&gt;
&lt;br /&gt;
If the body has the escape velocity with respect to the Earth, this is not enough to escape the Solar System, so near the Earth the orbit resembles a parabola, but further away it bends into an elliptical orbit around the Sun.&lt;br /&gt;
&lt;br /&gt;
This velocity (&amp;lt;math&amp;gt;v\,&amp;lt;/math&amp;gt;) is closely related to the [[orbital velocity]] of a body in a [[circular orbit]] of the radius equal to the radial position of orbiting body on the parabolic trajectory:&lt;br /&gt;
:&amp;lt;math&amp;gt;v=\sqrt{2}\cdot v_o&amp;lt;/math&amp;gt;&lt;br /&gt;
where:&lt;br /&gt;
*&amp;lt;math&amp;gt;v_o\,&amp;lt;/math&amp;gt; is [[orbital velocity]] of a body in [[circular orbit]].&lt;br /&gt;
&lt;br /&gt;
==Equation of motion==&lt;br /&gt;
Under standard assumptions, for a body moving along this kind of [[orbit|trajectory]] an [[orbital equation]] becomes:&lt;br /&gt;
:&amp;lt;math&amp;gt;r={{h^2}\over{\mu}}{{1}\over{1+\cos\nu}}&amp;lt;/math&amp;gt;&lt;br /&gt;
where:&lt;br /&gt;
*&amp;lt;math&amp;gt;r\,&amp;lt;/math&amp;gt; is radial distance of orbiting body from [[central body]],&lt;br /&gt;
*&amp;lt;math&amp;gt;h\,&amp;lt;/math&amp;gt; is [[specific angular momentum]] of the [[orbiting body]],&lt;br /&gt;
*&amp;lt;math&amp;gt;\nu\,&amp;lt;/math&amp;gt; is a [[true anomaly]] of the orbiting body,&lt;br /&gt;
*&amp;lt;math&amp;gt;\mu\,&amp;lt;/math&amp;gt; is the [[standard gravitational parameter]].&lt;br /&gt;
&lt;br /&gt;
==Energy==&lt;br /&gt;
Under standard assumptions, [[specific orbital energy]] (&amp;lt;math&amp;gt;\epsilon\,&amp;lt;/math&amp;gt;) of parabolic trajectory is zero, so the [[orbital energy conservation equation]] for this trajectory takes form:&lt;br /&gt;
:&amp;lt;math&amp;gt;\epsilon={v^2\over2}-{\mu\over{r}}=0&amp;lt;/math&amp;gt;&lt;br /&gt;
where:&lt;br /&gt;
*&amp;lt;math&amp;gt;v\,&amp;lt;/math&amp;gt; is [[orbital velocity]] of orbiting body,&lt;br /&gt;
*&amp;lt;math&amp;gt;r\,&amp;lt;/math&amp;gt; is radial distance of orbiting body from [[central body]],&lt;br /&gt;
*&amp;lt;math&amp;gt;\mu\,&amp;lt;/math&amp;gt; is the [[standard gravitational parameter]].&lt;br /&gt;
&lt;br /&gt;
This is entirely equivalent to the [[characteristic energy]] (square of the speed at infinity) being 0:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;C_3 = 0&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Barker&#039;s equation==&lt;br /&gt;
Barker&#039;s equation relates the time of flight to the true anomaly of a parabolic trajectory.&amp;lt;ref&amp;gt;{{cite book&lt;br /&gt;
 | last1 = Bate&lt;br /&gt;
 | first1 = Roger&lt;br /&gt;
 | last2 = Mueller&lt;br /&gt;
 | first2 = Donald&lt;br /&gt;
 | last3 = White&lt;br /&gt;
 | first3 = Jerry&lt;br /&gt;
 | title = Fundamentals of Astrodynamics&lt;br /&gt;
 | publisher = Dover Publications, Inc., New York&lt;br /&gt;
 | year = 1971&lt;br /&gt;
 | ISBN = 0-486-60061-0}} p 188&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
t - T = \frac{1}{2}\sqrt{\frac{p^{3}}{\mu}}\left (D + \frac{1}{3}D^{3}\right )&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Where:&lt;br /&gt;
*D = tan(ν/2), ν is the true anomaly of the orbit&lt;br /&gt;
*t is the current time in seconds&lt;br /&gt;
*T is the time of periapsis passage in seconds&lt;br /&gt;
*μ is the standard gravitational parameter&lt;br /&gt;
*p is the [[Conic section#Features|semi-latus rectum]] of the trajectory ( p = h&amp;lt;sup&amp;gt;2&amp;lt;/sup&amp;gt;/μ )&lt;br /&gt;
&lt;br /&gt;
More generally, the time between any two points on an orbit is&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
t_{f} - t_{0} = \frac{1}{2}\sqrt{\frac{p^{3}}{\mu}}\left (D_{f} + \frac{1}{3}D_{f}^{3} - D_{0} - \frac{1}{3}D_{0}^{3}\right )&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&lt;br /&gt;
Alternately, the equation can be expressed in terms of periapsis distance, in a parabolic orbit r&amp;lt;sub&amp;gt;p&amp;lt;/sub&amp;gt; = p/2:&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
t - T = \sqrt{\frac{2r_{p}^{3}}{\mu}}\left (D + \frac{1}{3}D^{3}\right )&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Unlike [[Kepler&#039;s equation]], which is used to solve for true anomalies in elliptical and hyperbolic trajectories, the true anomaly in Barker&#039;s equation can be solved directly for t. If the following substitutions are made&amp;lt;ref&amp;gt;&lt;br /&gt;
{{cite book&lt;br /&gt;
 | last1 = Montenbruck&lt;br /&gt;
 | first1 = Oliver&lt;br /&gt;
 | last2 = Pfleger&lt;br /&gt;
 | first2 = Thomas&lt;br /&gt;
 | title = Astronomy on the Personal Computer&lt;br /&gt;
 | publisher = Springer-Verlag Berlin Heidelberg&lt;br /&gt;
 | year = 2009&lt;br /&gt;
 | ISBN = 978-3-540-67221-0}} p 64&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
A = \frac{3}{2}\sqrt{\frac{\mu}{2r_{p}}}(t-T)&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
B = \sqrt[3]{A + \sqrt{A^{2}+1}}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
then&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
\nu = 2\arctan(B - 1/B)&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Radial parabolic trajectory==&lt;br /&gt;
A radial parabolic trajectory is a non-periodic [[Radial_trajectory|trajectory on a straight line]] where the relative velocity of the two objects is always the [[escape velocity]]. There are two cases: the bodies move away from each other or towards each other.&lt;br /&gt;
&lt;br /&gt;
There is a rather simple expression for the position as function of time:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;r=(4.5\mu t^2)^{1/3}\!\,&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
where &lt;br /&gt;
* μ is the [[standard gravitational parameter]]&lt;br /&gt;
* &amp;lt;math&amp;gt;t=0\!\,&amp;lt;/math&amp;gt; corresponds to the extrapolated time of the fictitious starting or ending at the center of the central body.&lt;br /&gt;
&lt;br /&gt;
At any time the average speed from &amp;lt;math&amp;gt;t=0\!\,&amp;lt;/math&amp;gt; is 1.5 times the current speed, i.e. 1.5 times the local escape velocity.&lt;br /&gt;
&lt;br /&gt;
To have &amp;lt;math&amp;gt;t=0\!\,&amp;lt;/math&amp;gt; at the surface, apply a time shift; for the Earth (and any other spherically symmetric body with the same average density) as central body this time shift is 6 minutes and 20 seconds; seven of these periods later the height above the surface is three times the radius, etc.&lt;br /&gt;
&lt;br /&gt;
==See also==&lt;br /&gt;
* [[Kepler orbit]]&lt;br /&gt;
&lt;br /&gt;
==References==&lt;br /&gt;
{{Reflist}}&lt;br /&gt;
&lt;br /&gt;
&amp;lt;!-- there is a navbox, such list was redundant --&amp;gt;&lt;br /&gt;
{{orbits}}&lt;br /&gt;
&lt;br /&gt;
{{DEFAULTSORT:Parabolic Trajectory}}&lt;br /&gt;
&lt;br /&gt;
[[Category:Orbits]]&lt;br /&gt;
&lt;br /&gt;
[[it:Traiettoria parabolica]]&lt;br /&gt;
[[ja:放物線軌道]]&lt;br /&gt;
[[pt:Trajetória parabólica]]&lt;br /&gt;
[[tr:Parabolik yörünge]]&lt;/div&gt;</summary>
		<author><name>PenelopRosenste</name></author>
	</entry>
	<entry>
		<id>https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=48315</id>
		<title>Main Page</title>
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		<updated>2014-08-13T00:47:37Z</updated>

		<summary type="html">&lt;p&gt;PenelopRosenste: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;In [[condensed matter physics]], the &#039;&#039;&#039;Fermi surface&#039;&#039;&#039; is an abstract boundary in [[reciprocal space]] useful for predicting the thermal, electrical, magnetic, and optical properties of [[metal]]s, [[semimetal]]s, and doped [[semiconductor]]s. The shape of the Fermi surface is derived from the periodicity and symmetry of the [[crystalline lattice]] and from the occupation of [[electronic band structure|electronic energy bands]].    The existence of a Fermi surface is a direct consequence of the [[Pauli exclusion principle]], which allows a maximum of two electrons per quantum state.&lt;br /&gt;
&lt;br /&gt;
==Theory==&lt;br /&gt;
Consider a spinless ideal [[Fermi gas]] of &amp;lt;math&amp;gt;N&amp;lt;/math&amp;gt; particles. According to [[Fermi–Dirac statistics]], the mean occupation number of a state with energy &amp;lt;math&amp;gt;\epsilon_i&amp;lt;/math&amp;gt; is given by&amp;lt;ref name=&#039;Reif1965dist341&#039;&amp;gt;{{harv|Reif|1965|p=341}}&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;\langle n_i\rangle =\frac{1}{e^{(\epsilon_i-\mu)/k_BT}+1},&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
where,&lt;br /&gt;
&lt;br /&gt;
*&amp;lt;math&amp;gt;\left\langle n_i\right\rangle&amp;lt;/math&amp;gt; is the mean occupation number&lt;br /&gt;
&lt;br /&gt;
*&amp;lt;math&amp;gt;\epsilon_i&amp;lt;/math&amp;gt; is the kinetic energy of the &amp;lt;math&amp;gt;i^{th}&amp;lt;/math&amp;gt; state&lt;br /&gt;
&lt;br /&gt;
*&amp;lt;math&amp;gt;\mu&amp;lt;/math&amp;gt; is the &#039;&#039;[[internal chemical potential]]&#039;&#039; (at zero temperature, this is the maximum kinetic energy the particle can have, i.e. [[Fermi energy]] &amp;lt;math&amp;gt;\epsilon_F&amp;lt;/math&amp;gt;)&lt;br /&gt;
&lt;br /&gt;
Suppose we consider the limit &amp;lt;math&amp;gt;T\to 0&amp;lt;/math&amp;gt;. Then we have,&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;\left\langle n_i\right\rangle\approx\begin{cases}1 &amp;amp; (\epsilon_i&amp;lt;\mu) \\ 0 &amp;amp; (\epsilon_i&amp;gt;\mu)\end{cases}.&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
By the [[Pauli exclusion principle]], no two fermions can be in the same state. Therefore, in the state of lowest energy, the particles fill up all energy levels below &amp;lt;math&amp;gt;\epsilon_F&amp;lt;/math&amp;gt;, which is equivalent to saying that &#039;&#039;&amp;lt;math&amp;gt;\epsilon_F&amp;lt;/math&amp;gt; is the energy level below which there are exactly &amp;lt;math&amp;gt;N&amp;lt;/math&amp;gt; states.&lt;br /&gt;
&lt;br /&gt;
In momentum space, these particles fill up a sphere of radius &amp;lt;math&amp;gt;p_F&amp;lt;/math&amp;gt;, the surface of which is called the &#039;&#039;&#039;Fermi surface&#039;&#039;&#039;&amp;lt;ref&amp;gt;K. Huang, &#039;&#039;Statistical Mechanics&#039;&#039; (2000), p244&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
The linear response of a metal to an electric, magnetic or thermal gradient is determined by the shape of the Fermi surface, because currents are due to changes in the occupancy of states near the Fermi energy. Free-electron Fermi surfaces are spheres of radius&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;k_F = \frac{\sqrt{2 m E_F}} {\hbar}&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
determined by the valence electron concentration where &amp;lt;math&amp;gt;\hbar&amp;lt;/math&amp;gt; is the [[reduced Planck&#039;s constant]].   A material whose Fermi level falls in a gap between bands is an [[Electrical insulation|insulator]] or semiconductor depending on the size of the [[bandgap]].   When a material&#039;s Fermi level falls in a bandgap, there is no Fermi surface.&lt;br /&gt;
&lt;br /&gt;
[[Image:graphiteFS.png|thumb|A view of the [[graphite]] Fermi surface at the corner H points of the&lt;br /&gt;
[[Brillouin zone]] showing the trigonal symmetry of the electron and&lt;br /&gt;
hole pockets.]]&lt;br /&gt;
&lt;br /&gt;
Materials with complex crystal structures can have quite intricate Fermi surfaces.   The figure illustrates the [[anisotropic]] Fermi surface of graphite, which has both electron and hole pockets in its Fermi surface due to multiple bands crossing the Fermi energy along the &amp;lt;math&amp;gt;\vec{k}_z&amp;lt;/math&amp;gt; direction. Often in a metal the Fermi surface radius &amp;lt;math&amp;gt;k_F&amp;lt;/math&amp;gt; is larger than the size of the first [[Brillouin zone]] which results in a portion of the Fermi surface lying in the second (or higher) zones.    As with the band structure itself, the Fermi surface can be displayed in an extended-zone scheme where &amp;lt;math&amp;gt;\vec{k}&amp;lt;/math&amp;gt; is allowed to have arbitrarily large values or a reduced-zone scheme where wavevectors are shown [[Modular arithmetic|modulo]] &amp;lt;math&amp;gt;\frac{2 \pi} {a}&amp;lt;/math&amp;gt; (in the 1-dimensional case) where a is the [[lattice constant]]. In the three-dimensional case the reduced zone scheme means that from any wavevector &amp;lt;math&amp;gt;\vec{k}&amp;lt;/math&amp;gt; there is an appropriate number of reciprocal lattice vectors &amp;lt;math&amp;gt;\vec{K}&amp;lt;/math&amp;gt; subtracted that the new &amp;lt;math&amp;gt;\vec{k}&amp;lt;/math&amp;gt; now is closer to the origin in &amp;lt;math&amp;gt;\vec{k}&amp;lt;/math&amp;gt;-space than to any &amp;lt;math&amp;gt;\vec{K}&amp;lt;/math&amp;gt;.  Solids with a large density of states at the Fermi level become unstable at low temperatures and tend to form [[ground state]]s where the condensation energy comes from opening a gap at the Fermi surface.    Examples of such ground states are [[superconductor]]s, [[ferromagnet]]s, [[Jahn–Teller effect|Jahn–Teller distortions]] and [[spin density wave]]s.&lt;br /&gt;
&lt;br /&gt;
The state occupancy of [[fermion]]s like electrons is governed by [[Fermi–Dirac statistics]] so at finite temperatures the Fermi surface is accordingly broadened.   In principle all fermion energy level populations are bound by a Fermi surface although the term is not generally used outside of condensed-matter physics.&lt;br /&gt;
&lt;br /&gt;
==Experimental determination==&lt;br /&gt;
Electronic Fermi surfaces have been measured through observation of the oscillation of transport properties in magnetic fields &amp;lt;math&amp;gt;H&amp;lt;/math&amp;gt;, for example the [[de Haas–van Alphen effect]] (dHvA)  and the [[Shubnikov–de Haas effect]] (SdH).  The former is an oscillation in [[magnetic susceptibility]] and the latter in [[resistivity]].  The oscillations are periodic versus &amp;lt;math&amp;gt;1/H&amp;lt;/math&amp;gt; and occur because of the quantization of energy levels in the plane perpendicular to a magnetic field, a phenomenon first predicted by [[Lev Landau]].  The new states are called Landau levels and  are separated by an energy &amp;lt;math&amp;gt;\hbar \omega_c&amp;lt;/math&amp;gt; where &amp;lt;math&amp;gt;\omega_c = eH/m^*c&amp;lt;/math&amp;gt; is called the [[electron cyclotron resonance|cyclotron frequency]], &amp;lt;math&amp;gt;e&amp;lt;/math&amp;gt; is the electronic charge, &amp;lt;math&amp;gt;m^*&amp;lt;/math&amp;gt; is the electron [[effective mass (solid-state physics)|effective mass]] and &amp;lt;math&amp;gt;c&amp;lt;/math&amp;gt; is the [[speed of light]].    In a famous result, [[Lars Onsager]] proved that the period of oscillation &amp;lt;math&amp;gt;\Delta H&amp;lt;/math&amp;gt; is related to the cross-section of the Fermi surface (typically given in &amp;lt;math&amp;gt;\AA^{-2}&amp;lt;/math&amp;gt;) perpendicular to the magnetic field direction &amp;lt;math&amp;gt;A_{\perp}&amp;lt;/math&amp;gt; by the equation &amp;lt;math&amp;gt;A_{\perp} = \frac{2 \pi e \Delta H}{\hbar c}&amp;lt;/math&amp;gt;. Thus the determination of the periods of oscillation for various applied field directions allows mapping of the Fermi surface.&lt;br /&gt;
&lt;br /&gt;
Observation of the dHvA and SdH oscillations requires magnetic fields large enough that the circumference of the cyclotron orbit is smaller than a [[mean free path]].  Therefore dHvA and SdH experiments are usually performed at high-field facilities like the [http://www.hfml.ru.nl/ High Field Magnet Laboratory] in Netherlands, [http://ghmfl.grenoble.cnrs.fr/ Grenoble High Magnetic Field Laboratory] in France, the [http://akahoshi.nims.go.jp/TML/english/ Tsukuba Magnet Laboratory] in Japan or the  [http://www.magnet.fsu.edu/ National High Magnetic Field Laboratory] in the United States.&lt;br /&gt;
&lt;br /&gt;
[[Image:Fermi surface of BSCCO exp.jpg|thumb| [[Fermi surface of BSCCO]] measured by [[ARPES]]. The experimental data shown as an intensity plot in yellow-red-black scale. Green dashed rectangle represents the [[Brillouin zone]] of the CuO2 plane of [[BSCCO]].]]&lt;br /&gt;
&lt;br /&gt;
The most direct experimental technique to resolve the electronic structure of crystals in the momentum-energy space (see [[reciprocal lattice]]), and, consequently, the Fermi surface, is the [[angle resolved photoemission spectroscopy]] ([[ARPES]]). An example of the [[Fermi surface of superconducting cuprates]] measured by [[ARPES]] is shown in figure.&lt;br /&gt;
&lt;br /&gt;
With [[positron annihilation]] the two photons carry the momentum of the electron away; as the momentum of a thermalized positron is negligible, in this way also information about the momentum distribution can be obtained. Because the positron can be [[polarized]], also the momentum distribution for the two [[Spin (physics)|spin]] states in magnetized materials can be obtained. Another advantage with de Haas–Van Alphen effect is that the technique can be applied to non-dilute alloys. In this way the first determination of a &#039;&#039;smeared Fermi surface&#039;&#039; in a 30% alloy was obtained in 1978.&lt;br /&gt;
&lt;br /&gt;
==See also==&lt;br /&gt;
*[[Fermi energy]]&lt;br /&gt;
*[[Brillouin zone]]&lt;br /&gt;
*[[Fermi surface of superconducting cuprates]]&lt;br /&gt;
*[[Kelvin probe force microscope]]&lt;br /&gt;
&lt;br /&gt;
==References==&lt;br /&gt;
{{reflist}}&lt;br /&gt;
*N. Ashcroft and N.D. Mermin, &#039;&#039;Solid-State Physics&#039;&#039;, ISBN 0-03-083993-9.&lt;br /&gt;
*W.A. Harrison, &#039;&#039;Electronic Structure and the Properties of Solids&#039;&#039;, ISBN 0-486-66021-4.&lt;br /&gt;
*[http://www.phys.ufl.edu/fermisurface/ VRML Fermi Surface Database]&lt;br /&gt;
*J. M. Ziman, &#039;&#039;Electrons in Metals: A short Guide to the Fermi Surface&#039;&#039; (Taylor &amp;amp; Francis, London, 1963), ASIN B0007JLSWS.&lt;br /&gt;
&lt;br /&gt;
==External links==&lt;br /&gt;
&lt;br /&gt;
[[Category:Condensed matter physics]]&lt;br /&gt;
[[Category:Electric and magnetic fields in matter]]&lt;br /&gt;
[[Category:Enrico Fermi|Surface]]&lt;/div&gt;</summary>
		<author><name>PenelopRosenste</name></author>
	</entry>
	<entry>
		<id>https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=46918</id>
		<title>Main Page</title>
		<link rel="alternate" type="text/html" href="https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=46918"/>
		<updated>2014-08-12T18:06:11Z</updated>

		<summary type="html">&lt;p&gt;PenelopRosenste: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;{{lowercase|title=sRGB}}&lt;br /&gt;
[[Image:Cie Chart with sRGB gamut by spigget.png|250px|right|thumb|CIE 1931 xy [[chromaticity diagram]] showing the [[gamut]] of the sRGB color space and location of the primaries. The D65 [[white point]] is shown in the center. The Planckian locus is shown with color temperatures labeled in [[kelvin]]. The outer curved boundary is the spectral (or monochromatic) locus, with wavelengths shown in nanometers (labeled in blue). Note that the colors in this displayed file are being specified using sRGB. Areas outside the triangle cannot be accurately colored because they are out of the gamut of sRGB therefore they have been interpreted. Also note how the D65 label is not an ideal 6500-kelvin [[blackbody]] because it is based on atmospheric filtered daylight.]]&lt;br /&gt;
&lt;br /&gt;
[[Image:SRGB gamma.svg|thumb|250px|right|Plot of the sRGB intensities versus sRGB numerical values (red), and this function&#039;s slope in log-log space (blue) which is the effective gamma at each point. Below a compressed value of 0.04045 or a linear intensity of 0.00313, the curve is linear so the gamma is 1. Behind the red curve is a dashed black curve showing an exact gamma = 2.2 power law.]]&lt;br /&gt;
&lt;br /&gt;
&#039;&#039;&#039;sRGB&#039;&#039;&#039; is a standard [[RGB color space]] created cooperatively by [[Hewlett-Packard|HP]] and [[Microsoft]] in 1996 for use on monitors, printers and the [[Internet]]. &lt;br /&gt;
&lt;br /&gt;
sRGB uses the [[Rec. 709|ITU-R BT.709]] primaries, the same as are used in studio monitors and [[HDTV]],&amp;lt;ref&amp;gt;{{cite book | title = Digital Video and HDTV: Algorithms and Interfaces | author = Charles A. Poynton | publisher = Morgan Kaufmann | year = 2003 | isbn = 1-55860-792-7 | url = http://books.google.com/books?id=ra1lcAwgvq4C&amp;amp;pg=RA1-PA239&amp;amp;dq=rec+709+smpte }}&amp;lt;/ref&amp;gt; and a transfer function ([[gamma correction|gamma curve]]) typical of [[Cathode ray tube|CRTs]]. This specification allowed sRGB to be directly displayed on typical CRT monitors of the time, a factor which greatly aided its acceptance.&lt;br /&gt;
&lt;br /&gt;
Unlike most other [[RGB color space]]s, the sRGB [[Gamma correction|gamma]] cannot be expressed as a single numerical value. The overall gamma is approximately 2.2, consisting of a linear (gamma 1.0) section near black, and a non-linear section elsewhere involving a 2.4 exponent and a gamma (slope of log output versus log input) changing from 1.0 through about 2.3.&lt;br /&gt;
&lt;br /&gt;
==Background==&lt;br /&gt;
&lt;br /&gt;
The sRGB color space has been endorsed by the [[World Wide Web Consortium|W3C]], [[Exif]], [[Intel]], [[Pantone]], [[Corel]], and many other industry players. It is used in proprietary and open [[graphics file format]]s, such as [[Scalable Vector Graphics|SVG]].&lt;br /&gt;
&lt;br /&gt;
The sRGB color space is well specified and is designed to match  typical home and office viewing conditions, rather than the darker environment typically used for commercial color matching.&lt;br /&gt;
&lt;br /&gt;
Much software is now designed with the assumption that an 8-bit-per-channel image file placed unchanged onto an 8-bit-per-channel display will appear much as the sRGB specification recommends. [[LCD]]s, [[Digital photography|digital cameras]], printers, and scanners all follow the sRGB standard. Devices which do not naturally follow sRGB (as older CRT monitors did) include compensating circuitry or software so that, in the end, they also obey this standard. For this reason, one can generally assume, in the absence of embedded profiles or any other information, that any 8-bit-per-channel image file or any 8-bit-per-channel image [[Application programming interface|API]] or device interface can be treated as being in the sRGB color space. However, when the correct displaying of an RGB color space is needed, [[color management]] usually must be employed.&lt;br /&gt;
&lt;br /&gt;
==The sRGB gamut==&lt;br /&gt;
&lt;br /&gt;
sRGB defines the chromaticities of the red, green, and blue [[primary color|primaries]], the colors where one of the three channels is nonzero and the other two are zero.  The [[gamut]] of chromaticities that can be represented in sRGB is the [[color triangle]] defined by these primaries. As with any [[RGB color space]], for non-negative values of R, G, and B it is not possible to represent colors outside this triangle, which is well inside the range of colors visible to a human.&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot; align=&amp;quot;left&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! [[CIE 1931 color space#The CIE xy chromaticity diagram|Chromaticity]]&lt;br /&gt;
! Red&lt;br /&gt;
! Green&lt;br /&gt;
! Blue&lt;br /&gt;
! White point&lt;br /&gt;
|-&lt;br /&gt;
| &#039;&#039;x&#039;&#039;&lt;br /&gt;
| 0.6400&lt;br /&gt;
| 0.3000&lt;br /&gt;
| 0.1500&lt;br /&gt;
| 0.3127&lt;br /&gt;
|-&lt;br /&gt;
| &#039;&#039;y&#039;&#039;&lt;br /&gt;
| 0.3300&lt;br /&gt;
| 0.6000&lt;br /&gt;
| 0.0600&lt;br /&gt;
| 0.3290&lt;br /&gt;
|-&lt;br /&gt;
| &#039;&#039;Y&#039;&#039;&lt;br /&gt;
| 0.2126&lt;br /&gt;
| 0.7152&lt;br /&gt;
| 0.0722&lt;br /&gt;
| 1.0000&lt;br /&gt;
|}&lt;br /&gt;
&lt;br /&gt;
[[Image:srgbnonlinearity.png|frame|right|104px|On an sRGB display, each solid bar should look as bright as the surrounding striped dither. (Note: must be viewed at original, 100% size)]]&lt;br /&gt;
&lt;br /&gt;
sRGB also defines a nonlinear transformation between the intensity of these primaries and the actual number stored. The curve is similar to the gamma response of a CRT display. It is more important to replicate this curve than the primaries to get correct display of an sRGB image. This nonlinear conversion means that sRGB is a reasonably efficient use of the values in an integer-based image file to display human-discernible light levels.&lt;br /&gt;
&lt;br /&gt;
sRGB is sometimes avoided by high-end print publishing professionals because its color gamut is not big enough, especially in the blue-green colors, to include all the colors that can be reproduced in [[CMYK]] printing.&lt;br /&gt;
&lt;br /&gt;
== Specification of the transformation ==&lt;br /&gt;
===The forward transformation (CIE xyY or CIE XYZ to sRGB)===&lt;br /&gt;
The first step in the calculation of sRGB tristimulus values from the [[CIE 1931 color space|CIE XYZ]] tristimulus values is a linear transformation, which may be carried out by a matrix multiplication.  The numerical values below match those in the official sRGB specification (IEC 61966-2-1:1999) and differ slightly from those in a publication by sRGB&#039;s creators.&amp;lt;ref name=orig_pub&amp;gt;{{cite web | url = http://www.w3.org/Graphics/Color/sRGB &amp;lt;!-- ALTERNATIVE URL: http://www.color.org/sRGB.xalter --&amp;gt; | title = A Standard Default Color Space for the Internet – sRGB, Version 1.10 | author = Michael Stokes, Matthew Anderson, Srinivasan Chandrasekar, Ricardo Motta | date = November 5, 1996}}&amp;lt;/ref&amp;gt; &lt;br /&gt;
&lt;br /&gt;
&#039;&#039;&#039;It&#039;s important to note that these linear RGB values are &#039;&#039;not&#039;&#039; the final result.&#039;&#039;&#039;&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\begin{bmatrix}&lt;br /&gt;
R_\mathrm{linear}\\G_\mathrm{linear}\\B_\mathrm{linear}\end{bmatrix}=&lt;br /&gt;
\begin{bmatrix}&lt;br /&gt;
3.2406&amp;amp;-1.5372&amp;amp;-0.4986\\&lt;br /&gt;
-0.9689&amp;amp;1.8758&amp;amp;0.0415\\&lt;br /&gt;
0.0557&amp;amp;-0.2040&amp;amp;1.0570&lt;br /&gt;
\end{bmatrix}&lt;br /&gt;
\begin{bmatrix}&lt;br /&gt;
X \\ &lt;br /&gt;
Y \\ &lt;br /&gt;
Z \end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Note also, that if the [[CIE xyY]] color space values are given (where &#039;&#039;x&#039;&#039;, &#039;&#039;y&#039;&#039; are the chromaticity coordinates and &#039;&#039;Y&#039;&#039; is the [[luminance]]), they must first be transformed to CIE XYZ tristimulus values by:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;X = Y  x / y,\,&amp;lt;/math&amp;gt;&lt;br /&gt;
:&amp;lt;math&amp;gt;Z = Y  (1- x - y)/y\,&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
The intermediate parameters &amp;lt;math&amp;gt;R_\mathrm{linear}&amp;lt;/math&amp;gt;, &amp;lt;math&amp;gt;G_\mathrm{linear}&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;B_\mathrm{linear}&amp;lt;/math&amp;gt; for in-gamut colors are defined to be in the range [0,1], which means that the initial &#039;&#039;X&#039;&#039;, &#039;&#039;Y&#039;&#039;, and &#039;&#039;Z&#039;&#039; values need to be similarly scaled (if you start with XYZ values going to 100 or so, divide them by 100 first, or apply the matrix and then scale by a constant factor to the [0,1] range).  The linear RGB values are usually clipped to that range, with display white represented as (1,1,1); the corresponding original XYZ values are such that white is [[CIE Standard Illuminant D65|D65]] with unit luminance (&#039;&#039;X&#039;&#039;,&#039;&#039;Y&#039;&#039;,&#039;&#039;Z&#039;&#039; = 0.9505, 1.0000, 1.0890). Calculations assume the 2° [[standard colorimetric observer]].&amp;lt;ref name=orig_pub/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
sRGB was designed to reflect a typical real-world monitor with a gamma of 2.2, and the following formula transforms the linear values into sRGB. Let &amp;lt;math&amp;gt;C_\mathrm{linear}&amp;lt;/math&amp;gt; be &amp;lt;math&amp;gt;R_\mathrm{linear}&amp;lt;/math&amp;gt;, &amp;lt;math&amp;gt;G_\mathrm{linear}&amp;lt;/math&amp;gt;, or &amp;lt;math&amp;gt;B_\mathrm{linear}&amp;lt;/math&amp;gt;, and &amp;lt;math&amp;gt;C_\mathrm{srgb}&amp;lt;/math&amp;gt; be &amp;lt;math&amp;gt;R_\mathrm{srgb}&amp;lt;/math&amp;gt;, &amp;lt;math&amp;gt;G_\mathrm{srgb}&amp;lt;/math&amp;gt; or &amp;lt;math&amp;gt;B_\mathrm{srgb}&amp;lt;/math&amp;gt;:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;C_\mathrm{srgb}=\begin{cases}&lt;br /&gt;
12.92C_\mathrm{linear}, &amp;amp; C_\mathrm{linear} \le 0.0031308\\&lt;br /&gt;
(1+a)C_\mathrm{linear}^{1/2.4}-a, &amp;amp; C_\mathrm{linear} &amp;gt; 0.0031308&lt;br /&gt;
\end{cases}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
*where &amp;lt;math&amp;gt;a = 0.055&amp;lt;/math&amp;gt;&lt;br /&gt;
These gamma-corrected values are in the range 0 to 1. If values in the range 0 to 255 are required, e.g. for video display or 8-bit graphics, the usual technique is to multiply by 255 and round to an integer.&lt;br /&gt;
&lt;br /&gt;
===The reverse transformation===&lt;br /&gt;
Again the sRGB component values &amp;lt;math&amp;gt;R_\mathrm{srgb}&amp;lt;/math&amp;gt;, &amp;lt;math&amp;gt;G_\mathrm{srgb}&amp;lt;/math&amp;gt;, &amp;lt;math&amp;gt;B_\mathrm{srgb}&amp;lt;/math&amp;gt; are in the range 0 to 1. (A range of 0 to 255 can simply be divided by 255).&lt;br /&gt;
:&amp;lt;math&amp;gt;C_\mathrm{linear}=&lt;br /&gt;
\begin{cases}\frac{C_\mathrm{srgb}}{12.92}, &amp;amp; C_\mathrm{srgb}\le0.04045\\&lt;br /&gt;
\left(\frac{C_\mathrm{srgb}+a}{1+a}\right)^{2.4}, &amp;amp; C_\mathrm{srgb}&amp;gt;0.04045&lt;br /&gt;
\end{cases}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
(where &amp;lt;math&amp;gt;C&amp;lt;/math&amp;gt; is &amp;lt;math&amp;gt;R&amp;lt;/math&amp;gt;, &amp;lt;math&amp;gt;G&amp;lt;/math&amp;gt;, or &amp;lt;math&amp;gt;B&amp;lt;/math&amp;gt;). Followed by a matrix multiplication of the linear values to get XYZ:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\begin{bmatrix}&lt;br /&gt;
X\\Y\\Z\end{bmatrix}=&lt;br /&gt;
\begin{bmatrix}&lt;br /&gt;
0.4124&amp;amp;0.3576&amp;amp;0.1805\\&lt;br /&gt;
0.2126&amp;amp;0.7152&amp;amp;0.0722\\&lt;br /&gt;
0.0193&amp;amp;0.1192&amp;amp;0.9505&lt;br /&gt;
\end{bmatrix}&lt;br /&gt;
\begin{bmatrix}&lt;br /&gt;
R_\mathrm{linear}\\ &lt;br /&gt;
G_\mathrm{linear}\\ &lt;br /&gt;
B_\mathrm{linear}\end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
== Theory of the transformation ==&lt;br /&gt;
&lt;br /&gt;
It is often casually stated that the [[gamma correction|decoding gamma]] for sRGB data is 2.2, yet the above transform shows an exponent of 2.4. This is because the net effect of the piecewise decomposition is necessarily a changing instantaneous gamma at each point in the range: it goes from gamma = 1 at zero to a gamma of 2.4 at maximum intensity with a median value being close to 2.2. The transformation was designed to approximate a gamma of about 2.2, but with a linear portion near zero to avoid having an infinite slope at &#039;&#039;K&#039;&#039;&amp;amp;nbsp;= 0, which can cause numerical problems. The continuity condition for the curve &amp;lt;math&amp;gt;C_\mathrm{linear}&amp;lt;/math&amp;gt; which is defined above as a piecewise function of &amp;lt;math&amp;gt;C_\mathrm{srgb}&amp;lt;/math&amp;gt;, is&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;\left(\frac{K_0+a}{1+a}\right)^\gamma=\frac{K_0}{\phi}.&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Solving with &amp;lt;math&amp;gt;\gamma = 2.4&amp;lt;/math&amp;gt; and the standard value &amp;lt;math&amp;gt;\phi=12.92&amp;lt;/math&amp;gt; yields two solutions, &amp;lt;math&amp;gt;K_0&amp;lt;/math&amp;gt; ≈ &amp;lt;math&amp;gt;0.0381548&amp;lt;/math&amp;gt; or &amp;lt;math&amp;gt;K_0&amp;lt;/math&amp;gt; ≈ &amp;lt;math&amp;gt;0.0404482&amp;lt;/math&amp;gt;. The IEC 61966-2-1 standard uses the rounded value &amp;lt;math&amp;gt;K_0=0.04045&amp;lt;/math&amp;gt;. However, if we impose the condition that the slopes match as well then we must have&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;\gamma\left(\frac{K_0+a}{1+a}\right)^{\gamma-1}\left(\frac{1}{1+a}\right)=\frac{1}{\phi}.&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
We now have two equations. If we take the two unknowns to be &amp;lt;math&amp;gt;K_0&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;\phi&amp;lt;/math&amp;gt; then we can solve to give&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;K_0=\frac{a}{\gamma-1},\ \ \ \phi=\frac{(1+a)^\gamma(\gamma-1)^{\gamma-1}}{(a^{\gamma-1})(\gamma^\gamma)}.&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Substituting &amp;lt;math&amp;gt;a=0.055&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;\gamma=2.4&amp;lt;/math&amp;gt; gives &amp;lt;math&amp;gt;K_0&amp;lt;/math&amp;gt; ≈ &amp;lt;math&amp;gt;0.0392857&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;\phi&amp;lt;/math&amp;gt; ≈ &amp;lt;math&amp;gt;12.9232102&amp;lt;/math&amp;gt;, with the corresponding linear-domain threshold at &amp;lt;math&amp;gt;K_0 / \phi&amp;lt;/math&amp;gt; ≈ &amp;lt;math&amp;gt;0.00303993&amp;lt;/math&amp;gt;. These values, rounded to &amp;lt;math&amp;gt;K_0=0.03928&amp;lt;/math&amp;gt;, &amp;lt;math&amp;gt;\phi=12.92321&amp;lt;/math&amp;gt;, and &amp;lt;math&amp;gt;K_0/\phi=0.00304&amp;lt;/math&amp;gt;, are sometimes used to describe sRGB conversion.&amp;lt;ref&amp;gt;{{cite book | title = Colour Engineering: Achieving Device Independent Colour | author = Phil Green and Lindsay W. MacDonald | publisher = John Wiley and Sons| url = http://books.google.com/books?id=tn09voxr6agC&amp;amp;pg=PA350&amp;amp;dq=srgb+0.03928+date:0-2002 | year = 2002 | isbn = 0-471-48688-4 }}&amp;lt;/ref&amp;gt; Publications by sRGB&#039;s creators&amp;lt;ref name=orig_pub/&amp;gt; rounded to &amp;lt;math&amp;gt;K_0=0.03928&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;\phi=12.92&amp;lt;/math&amp;gt;, resulting in a small discontinuity in the curve. Some authors adopted these values in spite of the discontinuity.&amp;lt;ref&amp;gt;{{cite book | title = Acquisition and Reproduction of Color Images: Colorimetric and Multispectral Approaches | author = Jon Y. Hardeberg | url = http://books.google.com/books?id=e2umTIdI2u4C&amp;amp;pg=PA40&amp;amp;dq=srgb+0.00304+date:0-2002 | publisher = Universal-Publishers.com | year = 2001 | isbn = 1-58112-135-0 }}&amp;lt;/ref&amp;gt; For the standard, the rounded value &amp;lt;math&amp;gt;\phi=12.92&amp;lt;/math&amp;gt; was kept and the &amp;lt;math&amp;gt;K_0&amp;lt;/math&amp;gt; value was recomputed to make the resulting curve continuous, as described above, resulting in a slope discontinuity from 12.92 below the intersection to 12.70 above.&lt;br /&gt;
&lt;br /&gt;
== Viewing environment ==&lt;br /&gt;
&lt;br /&gt;
{| class=&amp;quot;wikitable&amp;quot;&lt;br /&gt;
|-&lt;br /&gt;
! Parameter&lt;br /&gt;
! Value&lt;br /&gt;
|-&lt;br /&gt;
| Luminance level&lt;br /&gt;
| 80&amp;amp;nbsp;cd/m&amp;lt;sup&amp;gt;2&amp;lt;/sup&amp;gt;&lt;br /&gt;
|-&lt;br /&gt;
| Illuminant white point&lt;br /&gt;
| &#039;&#039;x&#039;&#039; = 0.3127, &#039;&#039;y&#039;&#039; = 0.3291 (D65)&lt;br /&gt;
|-&lt;br /&gt;
| Image surround reflectance&lt;br /&gt;
| 20% (~medium gray)&lt;br /&gt;
|-&lt;br /&gt;
| Encoding ambient illuminance level&lt;br /&gt;
| 64 lux&lt;br /&gt;
|-&lt;br /&gt;
| Encoding ambient white point&lt;br /&gt;
| &#039;&#039;x&#039;&#039; = 0.3457, &#039;&#039;y&#039;&#039; = 0.3585 (D50)&lt;br /&gt;
|-&lt;br /&gt;
| Encoding viewing flare&lt;br /&gt;
| 1.0%&lt;br /&gt;
|-&lt;br /&gt;
| Typical ambient illuminance level&lt;br /&gt;
| 200 lux&lt;br /&gt;
|-&lt;br /&gt;
| Typical ambient white point&lt;br /&gt;
| &#039;&#039;x&#039;&#039; = 0.3457, &#039;&#039;y&#039;&#039; = 0.3585 (D50)&lt;br /&gt;
|-&lt;br /&gt;
| Typical viewing flare&lt;br /&gt;
| 5.0%&lt;br /&gt;
|}&lt;br /&gt;
The sRGB specification assumes a dimly lit encoding (creation) environment with an ambient correlated color temperature (CCT) of 5000 K. It is interesting to note that this differs from the CCT of the illuminant (D65). Using D50 for both would have made the white point of most photographic paper appear excessively blue.&amp;lt;ref&amp;gt;{{cite book|url=http://books.google.com/books?id=jFl-3v9sSEUC&amp;amp;pg=PA121&amp;amp;lpg=PA121&amp;amp;dq=%22My+suggestion+is+to+calibrate+to+a+D65+white+point.%22|first=Andrew|last=Rodney|publisher=Focal Press|year=2005|isbn=978-0-240-80649-5|title=Color Management for Photographers|page=121|quote=[http://www.xrite.com/product_overview.aspx?ID=592&amp;amp;Action=Support&amp;amp;SupportID=3349 Why Calibrate Monitor to D65 When Light Booth is D50]}}&amp;lt;/ref&amp;gt; The other parameters, such as the luminance level, are representative of a typical CRT monitor.&lt;br /&gt;
&lt;br /&gt;
For optimal results, the [[International Color Consortium|ICC]] recommends using the encoding viewing environment (i.e., dim, diffuse lighting) rather than the less-stringent typical viewing environment.&amp;lt;ref name=orig_pub/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Usage==&lt;br /&gt;
{{Refimprove section|date=July 2010}}&lt;br /&gt;
{{CIE1931xy_gamut_comparison.svg}}&lt;br /&gt;
Due to the standardization of sRGB on the Internet, on computers, and on printers, many low- to medium-end consumer [[digital camera]]s and [[Image scanner|scanners]] use sRGB as the [[Default (computer science)|default]] (or only available) working color space. As the sRGB gamut meets or exceeds the gamut of a low-end [[inkjet printer]], an sRGB image is often regarded as satisfactory for home use. However, consumer-level [[Charge-coupled device|CCDs]] are typically uncalibrated, meaning that even though the image is being labeled as sRGB, one can&#039;t conclude that the image is color-accurate sRGB.&lt;br /&gt;
&lt;br /&gt;
If the color space of an image is unknown and it is an 8- to 16-bit image format, assuming it is in the sRGB color space is a safe choice. This allows a program to identify a color space for all images, which may be much easier and more reliable than trying to track the &amp;quot;unknown&amp;quot; color space. An [[ICC profile]] may be used; the ICC distributes three such profiles:&amp;lt;ref&amp;gt;[http://color.org/srgbprofiles.xalter sRGB profiles], ICC&amp;lt;/ref&amp;gt; a profile conforming to version 4 of the ICC specification, which they recommend, and two profiles conforming to version 2, which is still commonly used.&lt;br /&gt;
&lt;br /&gt;
Images intended for professional printing via a fully color-managed workflow, e.g. [[prepress]] output, sometimes use another color space such as [[Adobe RGB color space|Adobe RGB (1998)]], which allows for a wider gamut. If such images are to be used on the Internet they may be converted to sRGB using [[color management]] tools that are usually included with software that works in these other color spaces.&lt;br /&gt;
&lt;br /&gt;
The two dominant programming interfaces for 3D graphics, [[OpenGL]] and [[Microsoft Direct3D|Direct3D]], have both incorporated half part support for the sRGB color space by using sRGB&#039;s gamma curve.&lt;br /&gt;
OpenGL supports the [[Texture mapping|textures]] with sRGB gamma encoded color components (first introduced with [http://www.opengl.org/registry/specs/EXT/texture_sRGB.txt EXT_texture_sRGB extension], added to the core in OpenGL 2.1) and rendering into sRGB gamma encoded [[framebuffer]]s (first introduced with [http://www.opengl.org/registry/specs/EXT/framebuffer_sRGB.txt EXT_framebuffer_sRGB extension], added to the core in OpenGL 3.0). Direct3D supports sRGB gamma textures and rendering into sRGB gamma surfaces starting with DirectX 9. Correct [[mipmap]]ping and [[interpolation]] of sRGB gamma textures has direct hardware support in texturing units of most modern [[GPU]]s (for example nVidia GeForce 8 performs conversion from 8-bit texture to linear values before interpolating those values), and do not have any performance penalty.&amp;lt;ref&amp;gt;GPU Gems 3, section 24.4.1, http://http.developer.nvidia.com/GPUGems3/gpugems3_ch24.html&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==See also==&lt;br /&gt;
*[[RGB color space]]&lt;br /&gt;
*[[scRGB]]&lt;br /&gt;
&lt;br /&gt;
==References==&lt;br /&gt;
&lt;br /&gt;
&amp;lt;references/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
===Standards===&lt;br /&gt;
&lt;br /&gt;
*  IEC 61966-2-1:1999 is the official specification of sRGB.  It provides viewing environment, encoding, and [[colorimetric]] details.&lt;br /&gt;
* Amendment A1:2003 to IEC 61966-2-1:1999 describes an analogous sYCC encoding for [[YCbCr]] color spaces, an extended-[[gamut]] RGB encoding, and a [[CIELAB]] transformation.&lt;br /&gt;
* sRGB on [http://www.color.org/chardata/rgb/srgb.xalter www.color.org]&lt;br /&gt;
* The fourth working draft of IEC 61966-2-1 is available online, but is not the complete standard. It can be downloaded from [http://www2.units.it/ipl/students_area/imm2/files/Colore1/sRGB.pdf www2.units.it].&lt;br /&gt;
&lt;br /&gt;
==External links==&lt;br /&gt;
* [http://www.color.org/ International Color Consortium]&lt;br /&gt;
* [http://web.archive.org/web/20030124233043/http://www.srgb.com/ Archive copy of http://www.srgb.com], now unavailable, containing much information on the design, principles and use of sRGB&lt;br /&gt;
* [http://www.w3.org/Graphics/Color/sRGB A Standard Default Color Space for the Internet – sRGB] at [[World Wide Web Consortium|w3.org]]&lt;br /&gt;
* [http://oss.sgi.com/projects/ogl-sample/registry/EXT/texture_sRGB.txt OpenGL extension for sRGB gamma textures] at [[Silicon Graphics International|sgi.com]]&lt;br /&gt;
* [http://www.brucelindbloom.com/index.html?Eqn_RGB_XYZ_Matrix.html Conversion matrices for RGB vs. XYZ conversion]&lt;br /&gt;
* [http://ninedegreesbelow.com/photography/srgb-profile-comparison.html Will the Real sRGB Profile Please Stand Up?]&lt;br /&gt;
&lt;br /&gt;
{{Color space}}&lt;br /&gt;
&lt;br /&gt;
[[Category:Color space]]&lt;br /&gt;
[[Category:Film and video technology]]&lt;/div&gt;</summary>
		<author><name>PenelopRosenste</name></author>
	</entry>
	<entry>
		<id>https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=46289</id>
		<title>Main Page</title>
		<link rel="alternate" type="text/html" href="https://en.formulasearchengine.com/w/index.php?title=Main_Page&amp;diff=46289"/>
		<updated>2014-08-12T14:35:17Z</updated>

		<summary type="html">&lt;p&gt;PenelopRosenste: &lt;/p&gt;
&lt;hr /&gt;
&lt;div&gt;In [[linear algebra]], [[linear transformation]]s can be represented by [[matrix (math)|matrices]].  If &#039;&#039;T&#039;&#039; is a linear transformation mapping &#039;&#039;&#039;R&#039;&#039;&#039;&amp;lt;sup&amp;gt;&#039;&#039;n&#039;&#039;&amp;lt;/sup&amp;gt; to &#039;&#039;&#039;R&#039;&#039;&#039;&amp;lt;sup&amp;gt;&#039;&#039;m&#039;&#039;&amp;lt;/sup&amp;gt; and &amp;lt;math&amp;gt;\vec x&amp;lt;/math&amp;gt; is a [[column vector]] with &#039;&#039;n&#039;&#039; entries, then&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;T( \vec x ) = \mathbf{A} \vec x&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
for some &#039;&#039;m&#039;&#039;&amp;amp;times;&#039;&#039;n&#039;&#039; matrix &#039;&#039;&#039;A&#039;&#039;&#039;, called the &#039;&#039;&#039;transformation matrix of &#039;&#039;T&#039;&#039;&#039;&#039;&#039;.&lt;br /&gt;
There is an alternative expression of transformation matrices involving [[row vector]]s that is preferred by some authors.&lt;br /&gt;
== Uses ==&lt;br /&gt;
&lt;br /&gt;
Matrices allow arbitrary [[linear transformations]] to be represented in a consistent format, suitable for computation.  This also allows transformations to be concatenated easily (by multiplying their matrices).&lt;br /&gt;
&lt;br /&gt;
Linear transformations are not the only ones that can be represented by matrices.  Some transformations that are non-linear on a n-dimensional [[Euclidean space]] &#039;&#039;&#039;R&#039;&#039;&#039;&amp;lt;sup&amp;gt;&#039;&#039;n&#039;&#039;&amp;lt;/sup&amp;gt;, can be represented as linear transformations on the &#039;&#039;n&#039;&#039;+1-dimensional space &#039;&#039;&#039;R&#039;&#039;&#039;&amp;lt;sup&amp;gt;&#039;&#039;n&#039;&#039;+1&amp;lt;/sup&amp;gt;. These include both [[affine transformations]] (such as [[Translation (geometry)|translation]]) and [[projective transformation]]s. For this reason, 4x4 transformation matrices are widely used in [[3D computer graphics]]. These &#039;&#039;n&#039;&#039;+1-dimensional transformation matrices are called, depending on their application, &#039;&#039;affine transformation matrices&#039;&#039;, &#039;&#039;projective transformation matrices&#039;&#039;, or more generally &#039;&#039;non-linear transformation matrices&#039;&#039;.  With respect to an &#039;&#039;n&#039;&#039;-dimensional matrix, an &#039;&#039;n&#039;&#039;+1-dimensional matrix can be described as an [[augmented matrix]].&lt;br /&gt;
&lt;br /&gt;
In the [[physics|physical sciences]], an [[active transformation]] is one which actually changes the physical position of a [[system]], and makes sense even in the absence of a [[coordinate system]] whereas a [[passive transformation]] is a change in the coordinate description of the physical system ([[change of basis]]). The distinction between active and passive [[Transformation (mathematics)|transformation]]s is important. By default, by &#039;&#039;transformation&#039;&#039;, [[mathematician]]s usually mean active transformations, while [[physicist]]s could mean either.&lt;br /&gt;
&lt;br /&gt;
Put differently, a &#039;&#039;passive&#039;&#039; transformation refers to observation of the &#039;&#039;same&#039;&#039; event from two different coordinate frames.&lt;br /&gt;
&lt;br /&gt;
==Finding the matrix of a transformation==&lt;br /&gt;
&lt;br /&gt;
If one has a linear transformation &amp;lt;math&amp;gt;T(x)&amp;lt;/math&amp;gt; in functional form, it is easy to determine the transformation matrix &#039;&#039;&#039;A&#039;&#039;&#039; by simply transforming each of the vectors of the [[standard basis]] by &#039;&#039;T&#039;&#039; and then inserting the results into the columns of a matrix.  In other words,&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;\mathbf{A} = \begin{bmatrix} T( \vec e_1 ) &amp;amp; T( \vec e_2 ) &amp;amp; \cdots &amp;amp; T( \vec e_n ) \end{bmatrix}&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
For example, the function &amp;lt;math&amp;gt;T(x) = 5x&amp;lt;/math&amp;gt; is a linear transformation.  Applying the above process (suppose that &#039;&#039;n&#039;&#039; = 2 in this case) reveals that&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;T( \vec{x} ) = 5 \vec{x} = 5 \mathbf{I} \vec{x} = \begin{bmatrix} 5 &amp;amp;&amp;amp; 0 \\ 0 &amp;amp;&amp;amp; 5 \end{bmatrix} \vec{x}&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==Examples in 2D graphics==&lt;br /&gt;
&lt;br /&gt;
Most common geometric transformations that keep the origin fixed are linear, including rotation, scaling, shearing, reflection, and orthogonal projection; if an affine transformation is not a pure translation it keeps some point fixed, and that point can be chosen as origin to make the transformation linear.  In two dimensions, linear transformations can be represented using a 2&amp;amp;times;2 transformation matrix.&lt;br /&gt;
&lt;br /&gt;
===Rotation===&lt;br /&gt;
&lt;br /&gt;
For [[coordinate rotation|rotation]] by an angle θ &#039;&#039;&#039;counter clockwise&#039;&#039;&#039; about the origin, the functional form is &amp;lt;math&amp;gt;x&#039; = x \cos \theta - y \sin \theta&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;y&#039; = x \sin \theta + y \cos \theta&amp;lt;/math&amp;gt;.  Written in matrix form, this becomes:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\begin{bmatrix} x&#039; \\ y&#039; \end{bmatrix} = \begin{bmatrix} \cos \theta &amp;amp;  -\sin\theta \\ \sin \theta &amp;amp; \cos \theta \end{bmatrix} \begin{bmatrix} x \\ y \end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Similarly, for a rotation &#039;&#039;&#039;clockwise&#039;&#039;&#039; about the origin, the functional form is &amp;lt;math&amp;gt;x&#039; = x \cos \theta + y \sin \theta&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;y&#039; = - x \sin \theta + y \cos \theta&amp;lt;/math&amp;gt; and the matrix form is:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\begin{bmatrix} x&#039; \\ y&#039; \end{bmatrix} = \begin{bmatrix} \cos \theta &amp;amp;  \sin\theta \\ -\sin \theta &amp;amp; \cos \theta \end{bmatrix} \begin{bmatrix} x \\ y \end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
===Scaling===&lt;br /&gt;
&lt;br /&gt;
For [[scaling (geometry)|scaling]] (that is, enlarging or shrinking), we have &amp;lt;math&amp;gt;x&#039; = s_x \cdot x&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;y&#039; = s_y \cdot y&amp;lt;/math&amp;gt;.  The matrix form is:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\begin{bmatrix} x&#039; \\ y&#039; \end{bmatrix} = \begin{bmatrix} s_x &amp;amp; 0 \\ 0 &amp;amp; s_y \end{bmatrix} \begin{bmatrix} x \\ y \end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
When &amp;lt;math&amp;gt;\ s_x s_y = 1&amp;lt;/math&amp;gt;, then the matrix is a [[squeeze mapping]] and preserves [[area]]s in the plane.&lt;br /&gt;
&lt;br /&gt;
===Shearing===&lt;br /&gt;
&lt;br /&gt;
For [[shear mapping]] (visually similar to slanting), there are two possibilities.&lt;br /&gt;
&lt;br /&gt;
A shear parallel to the &#039;&#039;x&#039;&#039; axis has &amp;lt;math&amp;gt;x&#039; = x + ky&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;y&#039; = y&amp;lt;/math&amp;gt;. Written in matrix form, this becomes:&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\begin{bmatrix} x&#039; \\ y&#039; \end{bmatrix} = \begin{bmatrix} 1 &amp;amp; k \\ 0 &amp;amp; 1 \end{bmatrix} \begin{bmatrix} x \\ y \end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
A shear parallel to the &#039;&#039;y&#039;&#039; axis has &amp;lt;math&amp;gt;x&#039; = x&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;y&#039; = y + kx&amp;lt;/math&amp;gt;, which has matrix form:&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\begin{bmatrix} x&#039; \\ y&#039; \end{bmatrix} = \begin{bmatrix} 1 &amp;amp; 0 \\ k &amp;amp; 1 \end{bmatrix} \begin{bmatrix} x \\ y \end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
===Reflection ===&lt;br /&gt;
&lt;br /&gt;
To reflect a vector about a line that goes through the origin, let &amp;lt;math&amp;gt;\scriptstyle \vec{l} = (l_x, l_y)&amp;lt;/math&amp;gt; be a [[vector (geometric)|vector]] in the direction of the line:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\mathbf{A} = \frac{1}{\lVert\vec{l}\rVert^2} \begin{bmatrix} l_x^2 - l_y^2 &amp;amp; 2 l_x l_y \\ 2 l_x l_y &amp;amp; l_y^2 - l_x^2 \end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
To reflect a point through a plane &amp;lt;math&amp;gt;ax + by + cz = 0&amp;lt;/math&amp;gt; (which goes through the origin), one can use &amp;lt;math&amp;gt;\mathbf{A} = \mathbf{I}-2\mathbf{NN}^T &amp;lt;/math&amp;gt;, where &amp;lt;math&amp;gt;\mathbf{I}&amp;lt;/math&amp;gt; is the 3x3 identity matrix and &amp;lt;math&amp;gt;\mathbf{N}&amp;lt;/math&amp;gt; is the three-dimensional [[unit vector]] for the surface normal of the plane.  If the [[L2 norm]] of &amp;lt;math&amp;gt;a, b,&amp;lt;/math&amp;gt; and &amp;lt;math&amp;gt;c&amp;lt;/math&amp;gt; is unity, the transformation matrix can be expressed as:&lt;br /&gt;
&lt;br /&gt;
&amp;lt;math&amp;gt;&lt;br /&gt;
\mathbf{A} = \begin{bmatrix} 1 - 2 a^2  &amp;amp; - 2 a b &amp;amp; - 2 a c \\ - 2 a b  &amp;amp; 1 - 2 b^2 &amp;amp; - 2 b c  \\ - 2 a c &amp;amp; - 2 b c &amp;amp; 1 - 2c^2 \end{bmatrix} &lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Note that these are particular cases of a [[Householder reflection]] in two and three dimensions.  A reflection about a line or plane that does not go through the origin is not a linear transformation; it is an [[affine transformation]].&lt;br /&gt;
&lt;br /&gt;
===Orthogonal projection===&lt;br /&gt;
&lt;br /&gt;
To project a vector orthogonally onto a line that goes through the origin, let &amp;lt;math&amp;gt;\scriptstyle \vec{u} \,=\, (u_x, u_y)&amp;lt;/math&amp;gt; be a [[vector (geometric)|vector]] in the direction of the line.  Then use the transformation matrix:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\mathbf{A} = \frac{1}{\lVert\vec{u}\rVert^2} \begin{bmatrix} u_x^2 &amp;amp; u_x u_y \\ u_x u_y &amp;amp; u_y^2 \end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
As with reflections, the orthogonal projection onto a line that does not pass through the origin is an affine, not linear, transformation.&lt;br /&gt;
&lt;br /&gt;
[[Projection (linear algebra)|Parallel projection]]s are also linear transformations and can be represented simply by a matrix.  However, perspective projections are not, and to represent these with a matrix, [[Homogeneous_coordinates#Use_in_computer_graphics|homogeneous coordinates]] must be used.&lt;br /&gt;
&lt;br /&gt;
==Composing and inverting transformations==&lt;br /&gt;
&lt;br /&gt;
One of the main motivations for using matrices to represent linear transformations is that transformations can then be easily composed (combined) and inverted.&lt;br /&gt;
&lt;br /&gt;
Composition is accomplished by [[matrix multiplication]].  If &#039;&#039;&#039;A&#039;&#039;&#039; and &#039;&#039;&#039;B&#039;&#039;&#039; are the matrices of two linear transformations, then the effect of applying first &#039;&#039;&#039;A&#039;&#039;&#039; and then &#039;&#039;&#039;B&#039;&#039;&#039; to a vector &#039;&#039;x&#039;&#039; is given by:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;\mathbf{B}(\mathbf{A} \vec{x} ) = (\mathbf{BA}) \vec{x}&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
(This is called the [[Associative property]].)&lt;br /&gt;
In other words, the matrix of the combined transformation &#039;&#039;&#039;&#039;&#039;A&#039;&#039;&#039; followed by &#039;&#039;&#039;B&#039;&#039;&#039;&#039;&#039; is simply the product of the individual matrices.  Note that the multiplication is done in the opposite order from the English sentence: the matrix of &amp;quot;&#039;&#039;&#039;A&#039;&#039;&#039; followed by &#039;&#039;&#039;B&#039;&#039;&#039;&amp;quot; is &#039;&#039;&#039;BA&#039;&#039;&#039;, not &#039;&#039;&#039;AB&#039;&#039;&#039;.&lt;br /&gt;
&lt;br /&gt;
A consequence of the ability to compose transformations by multiplying their matrices is that transformations can also be inverted by simply [[Invertible matrix|inverting their matrices]].  So, &#039;&#039;&#039;A&#039;&#039;&#039;&amp;lt;sup&amp;gt;-1&amp;lt;/sup&amp;gt; represents the transformation that &amp;quot;undoes&amp;quot; &#039;&#039;&#039;A&#039;&#039;&#039;.&lt;br /&gt;
&lt;br /&gt;
==Other kinds of transformations==&lt;br /&gt;
&lt;br /&gt;
===Affine transformations===&amp;lt;!-- This section is linked from [[Affine transformation]] --&amp;gt;&lt;br /&gt;
To represent [[affine transformation]]s with matrices, we can use [[homogeneous coordinates]].  This means representing a 2-vector (&#039;&#039;x&#039;&#039;, &#039;&#039;y&#039;&#039;) as a 3-vector (&#039;&#039;x&#039;&#039;, &#039;&#039;y&#039;&#039;, 1), and similarly for higher dimensions.  Using this system, translation can be expressed with matrix multiplication.  The functional form &amp;lt;math&amp;gt;x&#039; = x + t_x&amp;lt;/math&amp;gt;; &amp;lt;math&amp;gt;y&#039; = y + t_y&amp;lt;/math&amp;gt; becomes:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\begin{bmatrix} x&#039; \\ y&#039; \\ 1 \end{bmatrix} = \begin{bmatrix} 1 &amp;amp; 0 &amp;amp; t_x \\ 0 &amp;amp; 1 &amp;amp; t_y \\ 0 &amp;amp; 0 &amp;amp; 1 \end{bmatrix} \begin{bmatrix} x \\ y \\ 1 \end{bmatrix}.&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
All ordinary linear transformations are included in the set of affine transformations, and can be described as a simplified form of affine transformations. Therefore, any linear transformation can be also represented by a general transformation matrix. The latter is obtained by expanding the corresponding linear transformation matrix by one row and column, filling the extra space with zeros except for the lower-right corner, which must be set to 1. For example, &#039;&#039;the &#039;&#039;&#039;anti-clockwise&#039;&#039;&#039; rotation matrix from above&#039;&#039; becomes:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;\begin{bmatrix} \cos \theta &amp;amp;  -\sin \theta &amp;amp; 0 \\ \sin \theta &amp;amp; \cos \theta &amp;amp; 0 \\ 0 &amp;amp; 0 &amp;amp; 1 \end{bmatrix}&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
Using transformation matrices containing homogeneous coordinates, translations can be seamlessly intermixed with all other types of transformations. The reason is that the real plane is mapped to the &#039;&#039;w&#039;&#039; = 1 plane in real projective space, and so translation in real [[Euclidean space]] can be represented as a shear in real projective space. Although a translation is a non-linear transformation in a 2-D or 3-D Euclidean space described by Cartesian coordinates, it becomes, in a 3-D or 4-D projective space described by homogeneous coordinates, a simple linear transformation (a shear).&lt;br /&gt;
&lt;br /&gt;
When using affine transformations, the homogeneous component of a coordinate vector (normally called &#039;&#039;w&#039;&#039;) will never be altered.  One can therefore safely assume that it is always 1 and ignore it.  However, this is not true when using perspective projections.&lt;br /&gt;
&lt;br /&gt;
===Perspective projection===&lt;br /&gt;
{{see also|3D projection#Perspective projection}}&lt;br /&gt;
Another type of transformation, of importance in [[3D computer graphics]], is the [[perspective projection]].  Whereas parallel projections are used to project points onto the image plane along parallel lines, the perspective projection projects points onto the image plane along lines that emanate from a single point, called the center of projection.  This means that an object has a smaller projection when it is far away from the center of projection and a larger projection when it is closer.&lt;br /&gt;
&lt;br /&gt;
The simplest perspective projection uses the origin as the center of projection, and &#039;&#039;z&#039;&#039; = 1 as the image plane.  The functional form of this transformation is then &amp;lt;math&amp;gt;x&#039; = x / z&amp;lt;/math&amp;gt;; &amp;lt;math&amp;gt;y&#039; = y / z&amp;lt;/math&amp;gt;.  We can express this in [[homogeneous coordinates]] as:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\begin{bmatrix} x_c \\ y_c \\ z_c \\ w_c \end{bmatrix} = &lt;br /&gt;
 \begin{bmatrix} 1 &amp;amp; 0 &amp;amp; 0 &amp;amp; 0 \\ 0 &amp;amp; 1 &amp;amp; 0 &amp;amp; 0 \\ 0 &amp;amp; 0 &amp;amp; 1 &amp;amp; 0 \\ 0 &amp;amp; 0 &amp;amp; 1 &amp;amp; 0 \end{bmatrix} \begin{bmatrix} x \\ y \\ z \\ 1 \end{bmatrix} =&lt;br /&gt;
 \begin{bmatrix} x \\ y \\ z \\ z \end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
After carrying out the matrix multiplication, the homogeneous component &#039;&#039;w&amp;lt;sub&amp;gt;c&amp;lt;/sub&amp;gt;&#039;&#039; will, in general, not be equal to 1.  Therefore, to map back into the real plane we must perform the &#039;&#039;&#039;homogeneous divide&#039;&#039;&#039; or &#039;&#039;&#039;perspective divide&#039;&#039;&#039; by dividing each component by &#039;&#039;w&amp;lt;sub&amp;gt;c&amp;lt;/sub&amp;gt;&#039;&#039;:&lt;br /&gt;
&lt;br /&gt;
:&amp;lt;math&amp;gt;&lt;br /&gt;
\begin{bmatrix} x&#039; \\ y&#039; \\ z&#039; \end{bmatrix} = \frac{1}{w_c} \begin{bmatrix} x_c \\ y_c \\ z_c \end{bmatrix}&lt;br /&gt;
&amp;lt;/math&amp;gt;&lt;br /&gt;
&lt;br /&gt;
More complicated perspective projections can be composed by combining this one with rotations, scales, translations, and shears to move the image plane and center of projection wherever they are desired.&lt;br /&gt;
&lt;br /&gt;
==See also==&lt;br /&gt;
* [[3D projection]]&lt;br /&gt;
* [[Transformation (geometry)]]&lt;br /&gt;
* [[Translation matrix]]&lt;br /&gt;
* [[Rotation matrix]]&lt;br /&gt;
* [[Scaling (geometry)]]&lt;br /&gt;
&lt;br /&gt;
==External links==&lt;br /&gt;
* [http://web.archive.org/web/20091027131421/http://geocities.com/evilsnack/matrix.htm  The Matrix Page] Practical examples in [[POV-Ray]]&lt;br /&gt;
* [http://mathworld.wolfram.com/RotationMatrix.html Reference page] - Rotation of axes&lt;br /&gt;
* [http://www.idomaths.com/linear_transformation.php Linear Transformation Calculator]&lt;br /&gt;
* [http://www.wiley.com/legacy/products/subject/life/biological_anthropology/0471205079_virtual_reconstruction/chapter5_trafo.html Transformation Applet] - Generate matrices from 2D transformations and vice versa.&lt;br /&gt;
&lt;br /&gt;
[[Category:Computer graphics]]&lt;br /&gt;
[[Category:Transformation (function)]]&lt;br /&gt;
[[Category:Matrices]]&lt;br /&gt;
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{{Unreferenced|date=December 2007}}&lt;br /&gt;
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[[de:Abbildungsmatrix]]&lt;br /&gt;
[[fr:Matrice de passage]]&lt;br /&gt;
[[it:Matrice di trasformazione]]&lt;br /&gt;
[[he:מטריצת מעבר]]&lt;br /&gt;
[[no:Transformasjonsmatrise]]&lt;br /&gt;
[[pl:Macierz przekształcenia liniowego]]&lt;br /&gt;
[[ru:Матрица перехода]]&lt;br /&gt;
[[sl:Matrika preslikave]]&lt;br /&gt;
[[uk:Матриця переходу]]&lt;br /&gt;
[[vi:Ma trận của biến đổi tuyến tính]]&lt;br /&gt;
[[zh:变换矩阵]]&lt;/div&gt;</summary>
		<author><name>PenelopRosenste</name></author>
	</entry>
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