<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">OJFD</journal-id><journal-title-group><journal-title>Open Journal of Fluid Dynamics</journal-title></journal-title-group><issn pub-type="epub">2165-3852</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ojfd.2013.34041</article-id><article-id pub-id-type="publisher-id">OJFD-41063</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  A New Large Scale Instability in Rotating Stratified Fluids Driven by Small Scale Forces
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>natoly</surname><given-names>Tur</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Malik</surname><given-names>Chabane</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Vladimir</surname><given-names>Yanovsky</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Institute for Single Crystals, National Academy of Science Ukraine, Kharkov, Ukraine</addr-line></aff><aff id="aff1"><addr-line>Université de Toulouse [UPS], Centre National de la Recherche Scientifique, 
Institut de Recherche en Astrophysique et Planétologie, Toulouse, France</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>anatoly.tour@irap.omp.eu(NT)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>15</day><month>11</month><year>2013</year></pub-date><volume>03</volume><issue>04</issue><fpage>340</fpage><lpage>351</lpage><history><date date-type="received"><day>October</day>	<month>25,</month>	<year>2013</year></date><date date-type="rev-recd"><day>November</day>	<month>25,</month>	<year>2013</year>	</date><date date-type="accepted"><day>December</day>	<month>3,</month>	<year>2013</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  In this paper, we find a new large scale instability displayed by a stratified rotating flow in forced turbulence. The tur
  bulence is generated by a small scale external force at low Reynolds number. The theory is built on the rigorous as
  ymptotic method of multi-scale development. There is no other special constraint concerning the force. In previous pa
  pers, the force was either helical or violating parity invariance. The nonlinear equations for the instability are obtained at the third order of the perturbation theory. In this article, we explain a detailed study of the linear stage of the instabil
  ity.
  
 
</p></abstract><kwd-group><kwd>Large Scale Vortex Instability; Coriolis Forse; Buoyancy; Multi-Scale Development; Small Scale Turbulence</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Large scale instabilities are very important in fluid dynamics. They generate vortices which play a fundamental role in turbulence and in transport processes. The characteristic dimensions of the large scale structures are greater than the typical scale of the turbulence. The turbulence is often simulated using a small scale external force. In this case, the large scale vortices are much greater than the scale of the external force. Large scale vortices are well observed in planetary atmospheres [1, 2], in numerical simulations, and in laboratory experiments [3-10]. The generation process of large scale instabilities has been studied in several papers [11-19]. In these papers, the turbulence which generates these coherent large scale structures cannot be homogenous, isotropic, or mirror invariant. A series of papers have shown that the essential mechanism which leads to the generation of large scale vortices is the lack of reflection invariance. This mechanism was called the hydrodynamic α-effect by analogy with the similar mechanism of generation of large scale magnetic fields.</p><p>Turbulence lacking reflection invariance is helical and a pseudo-scalar <img src="13-2320109\1a53d04c-65b7-4574-a816-7f6fd2306b11.jpg" /> appears. Nevertheless, the helicity of turbulence by itself can not generate large scale vortices. Other factors which lack reflection invariance are necessary, such as, for instance, compressibility [16,19] or temperature gradients [17,18]. Large scale instability can also appear if the turbulence lacks parity invariance (AKA effect) [<xref ref-type="bibr" rid="scirp.41063-ref12">12</xref>]. The helicity of the turbulence can be defined in a phenomenological way, but helicity can also be generated by an internal mechanism like rotation or buoyancy [13,15,20].</p><p>Large scale instabilities in a stratified rotating flow were studied in [21,22]. In [<xref ref-type="bibr" rid="scirp.41063-ref21">21</xref>], it was shown that a rotating incompressible flow with a constant temperature gradient can not display a large scale instability. In [<xref ref-type="bibr" rid="scirp.41063-ref22">22</xref>] the author presented large scale instabilities with a quadratic temperature gradient. In both papers, the authors used the functional averaging method. This method has some inconveniences. Especially it is impossible to make a strict hierarchy of orders as in perturbation theory. This means that it is impossible to identify the orders in which the instability appears and the ones in which it is absent. That is why the fact that the instability is absent when using the functional averaging method can not exclude its occurrence when using the rigorous asymptotic method of multi-scale development.</p><p>The occurrence of large scale instability in helical stratified turbulence was confirmed by the multi-scale development method in [<xref ref-type="bibr" rid="scirp.41063-ref23">23</xref>]. In that paper it was shown that the instability appears at the third order in the asymptotical development built on the small value of the Reynolds number. But in the first papers on this subject, using the functional averaging method, it was not clear in which order the instability would appear.</p><p>Direct numerical simulation of the Boussinesq Equation confirmed the existence of large scale vortex generation in stratified and rotating flows [24,25]. Sometimes the appearance of large scale vortex structures is accompanied by an inverse cascade of energy both in the threedimensional case (AKA-effect [<xref ref-type="bibr" rid="scirp.41063-ref26">26</xref>]), and in the quasi two-dimensional case [4,7,9,10]. One may say that the inverse cascade itself is also one of the mechanisms of the generation of large scale structures [5,27]. One of the important large scale instabilities in an incompressible fluid is the AKA effect (Anisotropic Kinetic Alpha effect) which was found in the work of Frisch, She and Sulem [<xref ref-type="bibr" rid="scirp.41063-ref11">11</xref>]. In this paper, the large scale instability appears under the impact of a small scale force in which parity is broken (with zero helicity). In a later paper [<xref ref-type="bibr" rid="scirp.41063-ref12">12</xref>], the inverse cascade of energy and the nonlinear mode of instability saturation were studied. Despite the fact that the broken parity is a more general notion than helicity, in fact, the helicity <img src="13-2320109\e38684a7-f50b-4059-9a5b-73955fa44f99.jpg" /> is the widespread mechanism of symmetry breaking in hydrodynamical flows. The injection of a helical external force into a hydrodynamic system has been studied in several papers [16,19]. As a result, it was understood that a small scale turbulence that is able to generate large scale perturbations can not be simply homogeneous, isotropic, and helical [<xref ref-type="bibr" rid="scirp.41063-ref28">28</xref>], but must have additional special properties. In some cases, the existence of a large scale instability has been shown (a vortex dynamo or the hydrodynamic <img src="13-2320109\63e1386d-77e1-460d-8a65-35a42e44f17a.jpg" />-effect). In the magneto hydrodynamics of a conductive fluid, the <img src="13-2320109\f0d2c993-3632-4fcb-adc8-c919bd4c05aa.jpg" />-effect is well known [<xref ref-type="bibr" rid="scirp.41063-ref29">29</xref>]. In particular, in [<xref ref-type="bibr" rid="scirp.41063-ref17">17</xref>] it was shown that a large scale instability exists in convective systems with small scale helical turbulence. These papers as well as the results of numerical modelling are described in detail in the review article [<xref ref-type="bibr" rid="scirp.41063-ref30">30</xref>], which is focused essentially on possible applications of these results to the issue of tropical cyclone origination. In this paper, we develop an analytical theory of the new large scale instability which generates large scale vortices in a stratified rotating flow with a constant temperature gradient under the action of a small scale external force which does not have any particular properties (especially it is nonhelical and it does not lack parity invariance). The force only maintains turbulent fluctuations. In other words, this force cannot display any instability. But the situation changes when both the Coriolis force and the buoyancy are added to this force. The joint action of these forces generates an internal helicity, which in turn generates an instability. The theory of this instability is developed rigourously using the method of asymptotic multi-scale development similar to what was done by Frisch, She and Sulem for the theory of the AKA effect [<xref ref-type="bibr" rid="scirp.41063-ref11">11</xref>]. This method allows finding the equations for large scale perturbations as the secular equations of perturbation theory, to calculate the Reynolds stress tensor and to find the instability. Our paper is organised as follows: In Section 2, we formulate the problem and the equations for the Coriolis force and the stratification in the Boussinesq approximation; In Section 3, we examine the principal scheme of the multi-scale development and we give the secular equations. In Section 4, we describe the calculations of the Reynolds stress. In Section 5, we discuss the instability and the conditions for its realization. The results obtained are discussed in the conclusions given in Section 6. The Reynolds stress and internal helicity are calculted in Appendices A and B, respectively.</p></sec><sec id="s2"><title>2. The Main Equations and Formulation of the Problem</title><p>Let us consider the equations for the motion of an incompressible fluid with a constant temperature gradient in the Boussinesq approximation:</p><disp-formula id="scirp.41063-formula31531"><label>(1)</label><graphic position="anchor" xlink:href="13-2320109\91920f29-e1e6-4d26-9b01-aed0950c8384.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31532"><label>(2)</label><graphic position="anchor" xlink:href="13-2320109\96204445-0acd-4a3f-924e-ae0ccc41481a.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31533"><label>(3)</label><graphic position="anchor" xlink:href="13-2320109\5137edc9-cf5e-4933-837a-71934e26ea0b.jpg"  xlink:type="simple"/></disp-formula><p>Here, <img src="13-2320109\822dc4f2-bfe0-4516-8954-d4c375422e9b.jpg" />, <img src="13-2320109\abc458f9-a2ca-4e16-b93f-ca5d71efafb2.jpg" />is the thermal expansion coefficient, <img src="13-2320109\88e85d7c-c83b-469c-b62e-e12266d69bb3.jpg" />is the constant equilibrium gradient of the temperature, <img src="13-2320109\9fff5455-67ad-401e-a9d6-6a076b4a547d.jpg" />, and<img src="13-2320109\1bc1865f-857a-4ca0-85f0-a3b8eaf0fd16.jpg" />. The external force <img src="13-2320109\cee785f5-bdc9-4c5b-b29b-4825f95e8c8e.jpg" /> has zero divergence. Let <img src="13-2320109\562b3b8d-5ffa-4205-990a-bf1c61f890f8.jpg" /> be, respectively, the characteristic scale, time, amplitude of the external force, and velocity of our system. We choose the dimensionless variables</p><p><img src="13-2320109\b5a885e7-876b-4ad5-b595-5c9f167ef6c1.jpg" /></p><p>Then,</p><p><img src="13-2320109\0ecb6633-4da4-4376-a6c4-91fed77eaac2.jpg" /></p><p>where <img src="13-2320109\bcd8042c-d9d0-44f0-acee-2b56670eb521.jpg" /> where R and <img src="13-2320109\1eea758b-d35c-45d2-9635-8b92d28fd226.jpg" /></p><p>are respectively the Reynolds number and the Taylor number on scale<img src="13-2320109\a0e06a9a-2bbf-46f3-b7f7-0af5b74c4695.jpg" />. <img src="13-2320109\a3069932-df1c-46dc-bb3e-a6a9317e5109.jpg" />represents the Prandtl number. We introduce the dimensionless temperature</p><p><img src="13-2320109\b106e802-6178-4ad9-b4ca-441a21f07356.jpg" />, and obtain the system of equations</p><p><img src="13-2320109\f8204d76-2778-4a01-bbfa-0a218cb477ea.jpg" /></p><p><img src="13-2320109\e2c91a67-6028-433b-9bd5-4e6f741b2038.jpg" /></p><p>Here, <img src="13-2320109\e3032297-d6e0-41bc-8e91-dd18a3383ede.jpg" />is the Rayleigh number on the scale<img src="13-2320109\6b46cdd8-4e42-451b-8c39-a89cbea7d973.jpg" />. Furthermore, for the purpose of simplification, we will consider the case<img src="13-2320109\fa1e00a6-c410-4814-8fd3-36cd9491ed12.jpg" />. We pass to the new temperature<img src="13-2320109\78440800-a22d-4815-90ae-04eea5ed8813.jpg" />, and obtain</p><disp-formula id="scirp.41063-formula31534"><label>(4)</label><graphic position="anchor" xlink:href="13-2320109\d313db3c-3694-4dd9-b814-6c72bdeeb7eb.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31535"><label>(5)</label><graphic position="anchor" xlink:href="13-2320109\88dffde0-3bfd-40dd-a15d-f446bcd0b7fc.jpg"  xlink:type="simple"/></disp-formula><p><img src="13-2320109\bdee4413-ea78-4f5d-b3e0-32fe8305f28c.jpg" /></p><p>We will consider as a small parameter of an asymptotic development the Reynolds number <img src="13-2320109\f4094716-b6a4-4e78-9352-a019e17fdbb4.jpg" /></p><p>on the scale<img src="13-2320109\afbc1a9d-df91-43a4-92df-ec937ac5c191.jpg" />. Concerning the parameters <img src="13-2320109\62b9d46a-0c57-435e-8963-0cf932e3f1c5.jpg" /> and<img src="13-2320109\bf1e58f9-2b4c-44aa-b4f0-ad765f9d22de.jpg" />, we do not choose any range of values for the moment. Let us examine the following formulation of the problem. We consider the external force as being small and of high frequency. This force leads to small scale fluctuations in velocity and temperature against a background of equilibrium. After averaging, these quickly oscillating fluctuations vanish. Nevertheless, due to small nonlinear interactions in some orders of perturbation theory, nonzero terms can occur after averaging. This means that they are not oscillatory, that is to say, they are large scale. From a formal point of view, these terms are secular, i.e., they create the conditions for the solvability of a large scale asymptotic development. So the purpose of this paper is to find and study the solvability equations, i.e., the equations for large scale perturbations. Let us denote the small scale variables by<img src="13-2320109\97274b97-6541-4454-98da-70e838e60078.jpg" />, and the large scale ones by<img src="13-2320109\c1d0a14c-05c5-45c0-a048-22f19007ff98.jpg" />. The small scale partial derivative operation<img src="13-2320109\c5080545-423d-4faf-8db5-560c2ca95965.jpg" />, and the large scale ones <img src="13-2320109\e7fb8121-af4b-4a5a-a630-508da133d1d8.jpg" /> are written, respectively, as <img src="13-2320109\6a9ef07b-a968-4879-affe-3811424a5e50.jpg" /></p><p>and<img src="13-2320109\59065316-9fbe-4334-aadc-e6e6bad8946b.jpg" />. To construct a multi-scale asymptotic development we follow the method which is proposed in [<xref ref-type="bibr" rid="scirp.41063-ref11">11</xref>].</p></sec><sec id="s3"><title>3. The Multi-Scale Asymptotic Development</title><p>Let us search for the solution to Equations (4) and (5) in the following form:</p><disp-formula id="scirp.41063-formula31536"><label>(6)</label><graphic position="anchor" xlink:href="13-2320109\570ae222-8715-4560-b0de-826a364e66af.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31537"><label>(7)</label><graphic position="anchor" xlink:href="13-2320109\df132808-acfe-4b85-876b-109f4f753f5b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31538"><label>(8)</label><graphic position="anchor" xlink:href="13-2320109\09e04147-00c8-48a2-bda4-f3bebe1a9fb5.jpg"  xlink:type="simple"/></disp-formula><p>Let us introduce the following equalities: <img src="13-2320109\60fa4aec-818e-42ce-8736-28dc33748532.jpg" />and <img src="13-2320109\e4ca6e54-4625-4370-8481-5de31c99f6cc.jpg" /> which lead to the expression for the space and time derivatives:</p><disp-formula id="scirp.41063-formula31539"><label>(9)</label><graphic position="anchor" xlink:href="13-2320109\16d9cbed-0fbe-4206-9526-368e569cea52.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31540"><label>(10)</label><graphic position="anchor" xlink:href="13-2320109\8c5a8a5b-78d7-4d7d-b32d-e9c7c2a0c8ee.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31541"><label>(11)</label><graphic position="anchor" xlink:href="13-2320109\a8c6d8cf-29fd-4443-90cb-7b326cacfe10.jpg"  xlink:type="simple"/></disp-formula><p>Using indicial notation, the system of the equation can be written as</p><disp-formula id="scirp.41063-formula31542"><label>(12)</label><graphic position="anchor" xlink:href="13-2320109\a7086f61-2817-4444-9d77-31ed644090a2.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31543"><label>(13)</label><graphic position="anchor" xlink:href="13-2320109\ad3e5fb2-19c5-4fa8-b81e-d5612dee8a5b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31544"><label>(14)</label><graphic position="anchor" xlink:href="13-2320109\40f3f79b-bcf5-4d1d-9af0-f1959f88a1a5.jpg"  xlink:type="simple"/></disp-formula><p>Substituting these expressions into the initial equations (4) and (5) and then gathering together the terms of the same order, we obtain the equations of the multiscale asymptotic development and write down the obtained equations up to order <img src="13-2320109\c73d056f-12ff-40e4-b367-1bf69099b69c.jpg" /> inclusive. In the order <img src="13-2320109\4b445a1f-2b5f-470b-84ae-0677c5e71d7b.jpg" /> there is only the Equation</p><disp-formula id="scirp.41063-formula31545"><label>(15)</label><graphic position="anchor" xlink:href="13-2320109\47a83386-ba3e-4d5e-acf2-267ae22a956e.jpg"  xlink:type="simple"/></disp-formula><p>In order <img src="13-2320109\afb45b31-a7b9-4db0-8e26-b9b44d7620c7.jpg" /> we have the equation</p><disp-formula id="scirp.41063-formula31546"><label>(16)</label><graphic position="anchor" xlink:href="13-2320109\69b7c903-f11c-4310-bf59-7ab185e729c4.jpg"  xlink:type="simple"/></disp-formula><p>In order <img src="13-2320109\17c0a3a3-8597-4e0c-b142-63c82f8b5a65.jpg" /> we get a system of equations:</p><disp-formula id="scirp.41063-formula31547"><label>(17)</label><graphic position="anchor" xlink:href="13-2320109\b6c9e7fe-4c2d-49cd-92d9-5b36bbfe813d.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31548"><label>(18)</label><graphic position="anchor" xlink:href="13-2320109\874d0120-447e-4a1f-b86e-c11bdf2056af.jpg"  xlink:type="simple"/></disp-formula><p><img src="13-2320109\3e142d39-cc2b-48f6-90d6-92b65b63779f.jpg" /></p><p>The system of Equations (17) and (18) gives the secular terms</p><disp-formula id="scirp.41063-formula31549"><label>(19)</label><graphic position="anchor" xlink:href="13-2320109\17194673-62b7-4ab6-95d6-e10c69bde8cd.jpg"  xlink:type="simple"/></disp-formula><p>which corresponds to a geostrophic equilibrum Equation, and</p><disp-formula id="scirp.41063-formula31550"><label>(20)</label><graphic position="anchor" xlink:href="13-2320109\27c5a53d-d416-4896-81bb-bda0a902c555.jpg"  xlink:type="simple"/></disp-formula><p>In zero order<img src="13-2320109\f780fa31-dedc-4e0f-b3bf-1d7bc1184417.jpg" />, we have the following system of equations:</p><disp-formula id="scirp.41063-formula31551"><label>(21)</label><graphic position="anchor" xlink:href="13-2320109\fffa0506-b0d5-448e-a899-6dd123e7af3b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31552"><label>(22)</label><graphic position="anchor" xlink:href="13-2320109\5a39d99d-2b07-472a-9651-567e838b1e42.jpg"  xlink:type="simple"/></disp-formula><p><img src="13-2320109\589e3899-d800-46e6-adab-36bd9c779b42.jpg" /></p><p>These equations give one secular Equation:</p><disp-formula id="scirp.41063-formula31553"><label>(23)</label><graphic position="anchor" xlink:href="13-2320109\88ed36ec-5922-43f6-ad70-e65bbcb40aa6.jpg"  xlink:type="simple"/></disp-formula><p>Let us consider the equations of the first approximation R:</p><disp-formula id="scirp.41063-formula31554"><label>(24)</label><graphic position="anchor" xlink:href="13-2320109\f51a1cb3-3444-4425-819f-0379e24b8b08.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31555"><label>(25)</label><graphic position="anchor" xlink:href="13-2320109\b4a7769c-fcf7-4299-aac7-987bd07d110b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31556"><label>(26)</label><graphic position="anchor" xlink:href="13-2320109\816401a2-5819-47a6-84f5-6b35afddb3f3.jpg"  xlink:type="simple"/></disp-formula><p>From this system of equations there follows the secular equations:</p><disp-formula id="scirp.41063-formula31557"><label>(27)</label><graphic position="anchor" xlink:href="13-2320109\b9a6b556-773a-47dc-a265-7f42f041485c.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31558"><label>(28)</label><graphic position="anchor" xlink:href="13-2320109\1e673096-a02e-4900-867f-8efa87bac56f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31559"><label>(29)</label><graphic position="anchor" xlink:href="13-2320109\4e9fc4ee-1c22-4958-aff3-d84c2f13106d.jpg"  xlink:type="simple"/></disp-formula><p>The secular equations (27) and (29) are satisfied by choosing the following geometry for the velocity field:</p><disp-formula id="scirp.41063-formula31560"><label>(30)</label><graphic position="anchor" xlink:href="13-2320109\559485b9-87e5-4ecc-94a2-82acee356741.jpg"  xlink:type="simple"/></disp-formula><p><img src="13-2320109\889850d9-332a-4fca-bcb9-ad949ef3781a.jpg" /></p><p>In the second order<img src="13-2320109\0ca231d5-c3d2-4c95-9b1f-26eb48d5e521.jpg" />, we obtain the equations</p><disp-formula id="scirp.41063-formula31561"><label>(31)</label><graphic position="anchor" xlink:href="13-2320109\5674a638-454b-4547-822a-59be6159074f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31562"><label>(32)</label><graphic position="anchor" xlink:href="13-2320109\659f1bc1-757e-4b34-bc2d-2f8102c340fe.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31563"><label>(33)</label><graphic position="anchor" xlink:href="13-2320109\2abe9e14-3220-4875-9411-37f1125c54ab.jpg"  xlink:type="simple"/></disp-formula><p>It is easy to see that there are no secular terms in this order..</p><p>Let us come now to the most important order<img src="13-2320109\34cfea91-596c-40b0-9311-d17c7182fc61.jpg" />. In this order we obtain the equations</p><disp-formula id="scirp.41063-formula31564"><label>(34)</label><graphic position="anchor" xlink:href="13-2320109\a4d7c8f0-e28b-4423-935f-6413a57fe21a.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31565"><label>(35)</label><graphic position="anchor" xlink:href="13-2320109\434239c5-cc8a-4910-bb54-3f159f7030ea.jpg"  xlink:type="simple"/></disp-formula><p><img src="13-2320109\0f58920e-47a2-428d-a809-cdeaad5bd798.jpg" /></p><p>From this we get the main secular Equation:</p><disp-formula id="scirp.41063-formula31566"><label>(36)</label><graphic position="anchor" xlink:href="13-2320109\494b04b4-3bea-47eb-8355-93c8d5422bee.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31567"><label>(37)</label><graphic position="anchor" xlink:href="13-2320109\f9c4a85d-d45e-40aa-ba52-ddb78658a05c.jpg"  xlink:type="simple"/></disp-formula><p>There is also an Equation to find the pressure<img src="13-2320109\a9bfefd0-3f2f-4389-a1cc-e51ab847fb57.jpg" />:</p><disp-formula id="scirp.41063-formula31568"><label>(38)</label><graphic position="anchor" xlink:href="13-2320109\50f35b67-8aff-48dd-8871-bb49d302369d.jpg"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. Calculations of the Reynolds Stresses</title><p>It is clear that the essential Equation for finding the nonlinear alpha-effect is Equation (36). In order to obtain these equations in closed form, we need to calculate the Reynolds stresses<img src="13-2320109\22fd82e7-2d20-448b-a84c-38167f6c16e3.jpg" />. First of all we have to calculate the fields of zero approximation<img src="13-2320109\f1a64590-f913-4369-81a5-43d873084f38.jpg" />. From the asymptotic development in zero order we have</p><disp-formula id="scirp.41063-formula31569"><label>(39)</label><graphic position="anchor" xlink:href="13-2320109\cee64c06-1a45-4ba4-a639-95aa36c9e0ae.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31570"><label>(40)</label><graphic position="anchor" xlink:href="13-2320109\5388b0f0-3846-46c0-8954-c307be4356ea.jpg"  xlink:type="simple"/></disp-formula><p>Let us introduce the operator<img src="13-2320109\24df279b-e4be-4ff2-9c50-50228ed457e0.jpg" />:</p><disp-formula id="scirp.41063-formula31571"><label>(41)</label><graphic position="anchor" xlink:href="13-2320109\a730412e-c9a5-4ff7-8c16-480aef8e8372.jpg"  xlink:type="simple"/></disp-formula><p>Using<img src="13-2320109\44b2b3d2-e9ac-4b93-aacd-38beaba98e99.jpg" />, we rewrite Equations (39) and (40):</p><disp-formula id="scirp.41063-formula31572"><label>(42)</label><graphic position="anchor" xlink:href="13-2320109\e0763c4d-2b7a-4ee5-a386-7a8b0a7f3990.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31573"><label>(43)</label><graphic position="anchor" xlink:href="13-2320109\4203524d-db81-4b64-9078-d5d612dfee3b.jpg"  xlink:type="simple"/></disp-formula><p>Eliminating the temperature and pressure from Equation (42), we obtain</p><disp-formula id="scirp.41063-formula31574"><label>(44)</label><graphic position="anchor" xlink:href="13-2320109\9a025a71-374b-46dc-b641-3e67eed1e15a.jpg"  xlink:type="simple"/></disp-formula><p>Here, <img src="13-2320109\509a2fff-ba26-4f7b-b59a-964e7d996e4f.jpg" />is the projection operator</p><p><img src="13-2320109\6a52792b-a269-462b-a492-b922dccea7bf.jpg" /></p><p>Dividing this equation by<img src="13-2320109\644daa17-db62-4c6e-b649-8500d181483e.jpg" />, we can write it in the form</p><disp-formula id="scirp.41063-formula31575"><label>(45)</label><graphic position="anchor" xlink:href="13-2320109\4107d79b-2a4e-4194-a01f-aa0268f2b33e.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="13-2320109\ffca05fd-e436-4ea3-a1fd-5daa0b3b1e63.jpg" /> is the operator given by</p><disp-formula id="scirp.41063-formula31576"><label>(46)</label><graphic position="anchor" xlink:href="13-2320109\636e6954-40e8-403a-9ff2-d72ac0ef6648.jpg"  xlink:type="simple"/></disp-formula><p>We must now determine the inverse operator <img src="13-2320109\ab618c68-b02c-4659-b452-2ce22f5bf7a7.jpg" /> <img src="13-2320109\65ed279f-1fd6-48b8-bbac-1803c98c4f9a.jpg" />: <img src="13-2320109\1ee2e645-76a2-47e7-93b3-21ea27a1e1f3.jpg" /></p><p>After some calculation, we find</p><disp-formula id="scirp.41063-formula31577"><label>(47)</label><graphic position="anchor" xlink:href="13-2320109\fdd13bec-e906-4407-b0d6-7a10185dceab.jpg"  xlink:type="simple"/></disp-formula><p>Here,</p><disp-formula id="scirp.41063-formula31578"><label>(48)</label><graphic position="anchor" xlink:href="13-2320109\d0855eff-49ea-43fa-95d4-b719a0274d19.jpg"  xlink:type="simple"/></disp-formula><p>and</p><p><img src="13-2320109\b2c48c96-4653-4401-bfdd-513588bb9e7f.jpg" /></p><p>Consequently, the expression for the velocity <img src="13-2320109\c14e5992-5585-404e-be37-6e78faf8d4e4.jpg" /> takes the form</p><disp-formula id="scirp.41063-formula31579"><label>(49)</label><graphic position="anchor" xlink:href="13-2320109\1360f32c-1302-4fa4-9a91-d559fca68173.jpg"  xlink:type="simple"/></disp-formula><p>In order to use these formulas, we have to specify in explicit form the external force<img src="13-2320109\1af3d723-ac8d-4cf5-a3d8-61733484c958.jpg" />. Let us specify it by</p><disp-formula id="scirp.41063-formula31580"><label>(50)</label><graphic position="anchor" xlink:href="13-2320109\f2f7eb89-5639-48f5-8dca-f160ed902c25.jpg"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.41063-formula31581"><label>(51)</label><graphic position="anchor" xlink:href="13-2320109\a0ca3e1c-7248-400d-b2c0-49d97da3ba2b.jpg"  xlink:type="simple"/></disp-formula><p>or</p><disp-formula id="scirp.41063-formula31582"><label>(52)</label><graphic position="anchor" xlink:href="13-2320109\29d704d0-2e47-4ed1-a432-4b09b1a7998f.jpg"  xlink:type="simple"/></disp-formula><p><img src="13-2320109\69f3b446-c1d6-4d1f-aa2c-7e6442293d7c.jpg" /></p><p>One can check that <img src="13-2320109\461c90c8-fd99-425b-be6c-f8e4be76db51.jpg" /> and <img src="13-2320109\aa5a5cf7-e519-416e-aead-8638dd37c6e1.jpg" /></p><p>Formulas (50) and (52) allow us to easily make intermediate calculations, but in the final formulas we obviously shall take <img src="13-2320109\76e9d7c3-ea55-4d86-9fd3-b2810f962af8.jpg" /> and <img src="13-2320109\8d68787d-f1c7-4000-9038-cd10ef7ffe43.jpg" /> as equal to unity, since the external force is dimensionless and depends only on the dimensionless arguments of space and time. The force (50) is physically simple and can be realized in laboratory experiments and in numerical simulations.</p><p>The force (50) can be written in complex form:</p><disp-formula id="scirp.41063-formula31583"><label>(53)</label><graphic position="anchor" xlink:href="13-2320109\992bf766-8310-429a-848a-0e9877618a0f.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="13-2320109\54678d37-c9b0-42ae-953e-a3ac5ec72e0b.jpg" /> and <img src="13-2320109\2d2b9951-5467-4d36-b9cb-429c834ec472.jpg" /> have the forms</p><disp-formula id="scirp.41063-formula31584"><label>(54)</label><graphic position="anchor" xlink:href="13-2320109\b47f4e1b-1ebe-4679-8380-04fb176acaa5.jpg"  xlink:type="simple"/></disp-formula><p>The effect of the operator <img src="13-2320109\717cc478-4dd0-4394-ac4c-41add2032670.jpg" /> on the proper function <img src="13-2320109\6d325b83-2430-4ea8-903d-9dbbb770b252.jpg" /> has obviously the form</p><p><img src="13-2320109\a6114096-7b4f-4440-bbfe-46629db23c06.jpg" />where <img src="13-2320109\02bcd2b8-8c3a-4ff9-81ea-7c502b7d2b75.jpg" /> is</p><disp-formula id="scirp.41063-formula31585"><label>(55)</label><graphic position="anchor" xlink:href="13-2320109\590ccd39-7fe5-4284-8832-eaf8719f6771.jpg"  xlink:type="simple"/></disp-formula><p>From this it follows that</p><disp-formula id="scirp.41063-formula31586"><label>(56)</label><graphic position="anchor" xlink:href="13-2320109\758ecadc-4bff-45dc-af0a-81884884ecba.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31587"><label>(57)</label><graphic position="anchor" xlink:href="13-2320109\5d1515ab-bfee-402f-93c0-2592ca9a98c9.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31588"><label>(58)</label><graphic position="anchor" xlink:href="13-2320109\d191d8cc-2b9f-40f7-9bef-8c5ad0866e50.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31589"><label>(59)</label><graphic position="anchor" xlink:href="13-2320109\112a2eb4-7184-4431-a56f-a6ad8fb5d3fd.jpg"  xlink:type="simple"/></disp-formula><p>From Formulas (49) and (53), it follows that the field <img src="13-2320109\75eef8b3-d945-475e-bdc5-22154a5a8370.jpg" /> is composed of four terms:</p><disp-formula id="scirp.41063-formula31590"><label>(60)</label><graphic position="anchor" xlink:href="13-2320109\f25030ec-568f-4f77-b695-683096443e84.jpg"  xlink:type="simple"/></disp-formula><p>where</p><p><img src="13-2320109\91060215-579c-430c-b59b-00110b2cadae.jpg" /></p><p>Finally, we introduce the notation</p><disp-formula id="scirp.41063-formula31591"><label>(61)</label><graphic position="anchor" xlink:href="13-2320109\013251b5-6f54-42d1-95c0-e6c4cf40627b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31592"><label>(62)</label><graphic position="anchor" xlink:href="13-2320109\7d60c1e9-a045-4658-b462-c6b5d71deaf7.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31593"><label>(63)</label><graphic position="anchor" xlink:href="13-2320109\14f57079-ba04-4945-af77-29e0e9518513.jpg"  xlink:type="simple"/></disp-formula><p><img src="13-2320109\91028296-2722-4177-988e-d57ca0352711.jpg" /></p><p>where<img src="13-2320109\f7eb61e1-0569-4deb-b80b-c6f6590a1271.jpg" />. Taking into account these formulas, we can write down the velocities <img src="13-2320109\9c996125-02cf-4f23-bd7f-dec88a96adeb.jpg" /> in the form</p><disp-formula id="scirp.41063-formula31594"><label>(64)</label><graphic position="anchor" xlink:href="13-2320109\8dc27746-1cd9-4cf9-9f00-7ccb400b24cd.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31595"><label>(65)</label><graphic position="anchor" xlink:href="13-2320109\16c2f89c-5518-49a3-933c-1f3ec7fbd8fd.jpg"  xlink:type="simple"/></disp-formula><p>where</p><p><img src="13-2320109\692b5503-3e77-4aea-a54e-6bc4a5b3d57f.jpg" /></p><p>and</p><p><img src="13-2320109\9c3c4b59-675b-4888-9fd0-74b947bf10d0.jpg" /></p><p>We can now calculate the Reynolds stresses:</p><disp-formula id="scirp.41063-formula31596"><label>(66)</label><graphic position="anchor" xlink:href="13-2320109\2be2399a-59fb-4a79-8580-435990f36bfa.jpg"  xlink:type="simple"/></disp-formula><p>which can be decomposed into two components:</p><disp-formula id="scirp.41063-formula31597"><label>(67)</label><graphic position="anchor" xlink:href="13-2320109\7f433541-68ef-4a67-8ff8-7c54d2ae93e0.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="13-2320109\000e19b5-9677-4ca7-830d-b86ea9ea3c09.jpg" /> and <img src="13-2320109\8d8398fe-ccfe-4549-9caf-1e70864200a8.jpg" /> can be expressed as follows:</p><disp-formula id="scirp.41063-formula31598"><label>(68)</label><graphic position="anchor" xlink:href="13-2320109\cd6a4e8d-12ff-4f79-ba64-4655acb73d75.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31599"><label>(69)</label><graphic position="anchor" xlink:href="13-2320109\cb0bd669-f267-4db3-8334-5ea2544fcf78.jpg"  xlink:type="simple"/></disp-formula><p>Taking into account Formulas (64) and (65), we obtain</p><p><img src="13-2320109\d0e422d0-44c4-4956-8156-ae2f73a1bb81.jpg" /></p><p>We can write down the components <img src="13-2320109\7098b4e7-727e-47e3-8c14-1987d097f61e.jpg" /> and<img src="13-2320109\6a9bb45a-008d-436b-83bb-54c3ec2ba19a.jpg" />, which are the ones of interest:</p><disp-formula id="scirp.41063-formula31600"><label>(70)</label><graphic position="anchor" xlink:href="13-2320109\44d53cc0-c443-412f-89d7-f7e16f3cddbd.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31601"><label>(71)</label><graphic position="anchor" xlink:href="13-2320109\fc1fcb2e-5fbe-4059-9e6d-ab852df6fc0f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31602"><label>(72)</label><graphic position="anchor" xlink:href="13-2320109\c4f7e1b3-1117-44b9-b917-e334819287b2.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31603"><label>(73)</label><graphic position="anchor" xlink:href="13-2320109\9d90d4d3-db17-4da5-b443-6f19cc8aefcb.jpg"  xlink:type="simple"/></disp-formula><p>Finally, using the following relations (we have similar formulas for <img src="13-2320109\10d98698-0a35-43a0-86c5-2418dd5c5b3c.jpg" /> after replacing <img src="13-2320109\18e25f24-c971-4f79-a800-d987017d1b2b.jpg" /> with<img src="13-2320109\e320cbbb-0f5a-4b07-a4c8-5dff1b9f3bc2.jpg" />):</p><disp-formula id="scirp.41063-formula31604"><label>(74)</label><graphic position="anchor" xlink:href="13-2320109\72e7a766-5a80-4758-a755-e18819c3a25c.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31605"><label>(75)</label><graphic position="anchor" xlink:href="13-2320109\ef6bd040-4b92-4da0-b004-8e84a45d10e2.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31606"><label>(76)</label><graphic position="anchor" xlink:href="13-2320109\719360ef-8874-427a-94bb-a0077d71c89d.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31607"><label>(77)</label><graphic position="anchor" xlink:href="13-2320109\fa45b811-e26a-426f-a382-75c8c2915868.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31608"><label>(78)</label><graphic position="anchor" xlink:href="13-2320109\dedfd635-d886-41a7-8f0c-776886483e12.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31609"><label>(79)</label><graphic position="anchor" xlink:href="13-2320109\18d80659-c708-4654-abda-036f37ca498f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31610"><label>(80)</label><graphic position="anchor" xlink:href="13-2320109\6d10fe48-d3fe-4bef-9bc4-4b4b260709f8.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31611"><label>(81)</label><graphic position="anchor" xlink:href="13-2320109\1bc371b7-2e55-457f-99e5-77a21082022e.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31612"><label>(82)</label><graphic position="anchor" xlink:href="13-2320109\228a8196-d8ed-45d2-8c38-cf5376da57dc.jpg"  xlink:type="simple"/></disp-formula><p>We can then express<img src="13-2320109\994d76d1-a5ed-435e-a3eb-4b0f57449c27.jpg" />, <img src="13-2320109\753dcb8b-71f9-472e-8299-a4695bddb8cc.jpg" />, <img src="13-2320109\631792e0-8458-4dcb-8040-7ffa076b8988.jpg" />and<img src="13-2320109\47128222-d19c-4018-a6e5-24f7be33b835.jpg" />:</p><p><img src="13-2320109\5d32bffa-0f0e-43c7-ba40-08767ad19cc8.jpg" /></p><p><img src="13-2320109\53a9efb3-5b09-4694-b18b-8216a03e06b5.jpg" /></p><p><img src="13-2320109\8472dac7-7b7a-44ec-8be6-b74f921ab31c.jpg" /></p><p><img src="13-2320109\7f533bdc-c595-45c9-9cb3-f4de2549a755.jpg" /></p><p>where</p></sec><sec id="s5"><title>5. Large Scale Instability</title><p>Let us write down in the explicit form the equations for nonlinear instability:</p><disp-formula id="scirp.41063-formula31613"><label>(83)</label><graphic position="anchor" xlink:href="13-2320109\06f39e78-fbee-41cd-986f-984d73035aa8.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31614"><label>(84)</label><graphic position="anchor" xlink:href="13-2320109\b5a0c394-bd10-4003-9882-e736b4c577f4.jpg"  xlink:type="simple"/></disp-formula><p>where the components<img src="13-2320109\68a1f0ba-54b4-4fce-86c8-db94421400eb.jpg" />, <img src="13-2320109\d1014a11-1729-4fc8-a5a4-221f29d0fecf.jpg" />, <img src="13-2320109\0571e090-21fb-4d71-90b0-a517c2e08b6e.jpg" />and <img src="13-2320109\bce0da0c-d723-44df-a1c8-11d95b1c8524.jpg" /> of the Reynolds stress tensor are as defined in the previous section.</p><p>One can see that for small values of the variables <img src="13-2320109\e94dcf03-dad1-4ed9-aa5c-5357ee3ab45a.jpg" /> and<img src="13-2320109\460d3881-137a-4a46-afc0-d2462a0467ee.jpg" />, Equations (83) and (84) are reduced to linear equations and describe the linear stage of instability:</p><disp-formula id="scirp.41063-formula31615"><label>(85)</label><graphic position="anchor" xlink:href="13-2320109\1acebff0-3a68-45da-8644-9458eaa32a38.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31616"><label>(86)</label><graphic position="anchor" xlink:href="13-2320109\5213f5e9-4a92-4f78-a4b8-482f465e2af5.jpg"  xlink:type="simple"/></disp-formula><p>where the coeficients<img src="13-2320109\098d7be5-1b78-4c44-8c62-d3c7b03e5f88.jpg" />, <img src="13-2320109\e082fe77-fdb7-4567-8a17-19fea0bc8b8a.jpg" />, <img src="13-2320109\db0afe4b-aa06-45c8-8177-bbf4d4f748f0.jpg" />and <img src="13-2320109\56d82375-aefb-4882-8116-8bd7695ecf2f.jpg" /> can be written as</p><disp-formula id="scirp.41063-formula31617"><label>(87)</label><graphic position="anchor" xlink:href="13-2320109\fcaef126-87f1-4783-b933-dab72491c349.jpg"  xlink:type="simple"/></disp-formula><p>with</p><disp-formula id="scirp.41063-formula31618"><label>(88)</label><graphic position="anchor" xlink:href="13-2320109\c3547335-34ac-413d-8c80-bc6d8ad264c9.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31619"><label>(89)</label><graphic position="anchor" xlink:href="13-2320109\b2d97697-75e6-49b7-8172-0b06d5f1d663.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31620"><label>(90)</label><graphic position="anchor" xlink:href="13-2320109\b58ada8d-ba91-44ac-b415-ef2a79efcfeb.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31621"><label>(91)</label><graphic position="anchor" xlink:href="13-2320109\5b0ac618-ca9e-448e-9af5-8bdee4684a8e.jpg"  xlink:type="simple"/></disp-formula><p>and</p><disp-formula id="scirp.41063-formula31622"><label>(92)</label><graphic position="anchor" xlink:href="13-2320109\8474b047-8ae3-49b3-8be0-9a84e052528b.jpg"  xlink:type="simple"/></disp-formula><p>which are the explicit forms of the quite bulky coefficients. However, these coefficients can be expressed using the internal helicity <img src="13-2320109\01731be4-d7a4-4043-a7e5-0d676a23bd0c.jpg" /> of the velocity field<img src="13-2320109\3336f42f-acc1-44da-b4ae-31a7c10323d2.jpg" />, calculated in Appendix B.</p><p><img src="13-2320109\e207cdcc-0606-4829-b38c-68a2a888c281.jpg" />.</p><p>Therefore, we can write the constant coefficients <img src="13-2320109\f4627541-01fc-4fe8-b26e-9141b12ceaef.jpg" /> and <img src="13-2320109\5409f94a-dcc4-4915-b884-8efa5774a5a4.jpg" /> with respect to<img src="13-2320109\c1da7738-1e3d-44df-b60d-b944be7cf53a.jpg" />:</p><p><img src="13-2320109\c9eb7e3f-5b32-4692-98ef-87f2967fbe37.jpg" /></p><p>where<img src="13-2320109\3c938749-dc2f-4e70-af68-9f18a9ebf4df.jpg" />.</p><p>Equations (85) and (86) can then be rewritten:</p><disp-formula id="scirp.41063-formula31623"><label>(93)</label><graphic position="anchor" xlink:href="13-2320109\5b0866d2-0e37-45bf-93b6-c65df2cf6b9b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31624"><label>(94)</label><graphic position="anchor" xlink:href="13-2320109\1889a799-afbe-4e4a-a63d-95e471e47b37.jpg"  xlink:type="simple"/></disp-formula><p>These formulas show that despite the zero helicity of the driving force, inside the system, an internal helicity is generated as a result of the joint impact of the Coriolis and buoyancy forces. This helicity plays an important role in the dynamics of the perturbations.</p><p>In order to find instabilities, we choose the velocity <img src="13-2320109\c43e00a6-0802-44b1-81bd-9f35572bd49e.jpg" /> in the form:</p><disp-formula id="scirp.41063-formula31625"><label>(95)</label><graphic position="anchor" xlink:href="13-2320109\a58dbecb-bcc9-4025-8e12-26655428ab35.jpg"  xlink:type="simple"/></disp-formula><p>Injecting these solutions into (85), we obtain the simple system of equations:</p><disp-formula id="scirp.41063-formula31626"><label>(96)</label><graphic position="anchor" xlink:href="13-2320109\61a3b8e2-7979-49d8-af41-bb885ebd31f9.jpg"  xlink:type="simple"/></disp-formula><p>Evidently we get a quadratic equation for<img src="13-2320109\f2100f6b-7e1b-45ae-b783-69937145f28b.jpg" />:</p><p><img src="13-2320109\9f271a20-0a77-4c68-a430-da34d710fda4.jpg" /></p><p>which allows us to obtain the dispersion equations for the different modes.</p><sec id="s6_0_1"><title>5.1.1. Dispersion Equation for the Unstable Mode</title><p>This equation is obtained by searching for solutions of (96) for which the discriminant is negative, namely,<img src="13-2320109\a24d2caf-f735-4e82-a471-6e962d803ae8.jpg" />. We show Figures 1 and 2 representing the area (in gray) of the plane <img src="13-2320109\1e2b26b2-0f6f-403f-a8a1-134f8891b014.jpg" /> for which the discriminant is negative, this means that an instability can appear. <xref ref-type="fig" rid="fig1">Figure 1</xref> shows the conditions for a negative temperature gradient and <xref ref-type="fig" rid="fig2">Figure 2</xref>, for a positive one.</p><p>Finally, we get</p><p><img src="13-2320109\12d7b5f0-9c2d-43d1-b740-9334cfca255f.jpg" /></p><p>where</p><disp-formula id="scirp.41063-formula31627"><label>(97)</label><graphic position="anchor" xlink:href="13-2320109\1929b94d-439d-432a-af13-02e0ae30b910.jpg"  xlink:type="simple"/></disp-formula><p>(97) is the growth rate of the instability. We note that it is proportionnal to the square of the helicity.</p></sec><sec id="s6_0_2"><title>5.1.2. Dispersion Equation for the Oscillatory Modes</title><p>This Equation is obtained by searching for solutions of (96) for which the discriminant is positive, namely,<img src="13-2320109\6f5f53d5-b962-4871-86df-7f8cf2f844b5.jpg" />.</p><p>We obtain in this case two oscillatory modes, <img src="13-2320109\d519cbbe-ea61-47c5-ad8c-fc96bae0528b.jpg" />and<img src="13-2320109\3a75ee34-d35b-495f-b24f-2a6b982af155.jpg" />, which are, respectively, a slow and a fast mode:</p><disp-formula id="scirp.41063-formula31628"><label>(98)</label><graphic position="anchor" xlink:href="13-2320109\897c9edf-22ca-4885-8661-e39a1727ecc7.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.41063-formula31629"><label>(99)</label><graphic position="anchor" xlink:href="13-2320109\a5717c8a-9107-4b80-858d-3f8e262f3ea9.jpg"  xlink:type="simple"/></disp-formula><p>It appears that both slow and fast oscillatory frequencies are proportional to the square of the helicity as well.</p></sec><sec id="s6_1"><title>5.2. Unstable and Oscillatory Modes with Viscosity</title><p>In the same way as before, we get the system</p><disp-formula id="scirp.41063-formula31630"><label>(100)</label><graphic position="anchor" xlink:href="13-2320109\1c8714c5-7bb7-4e3a-82fa-495312f7e09d.jpg"  xlink:type="simple"/></disp-formula><p>We can then get a new quadratic Equation for<img src="13-2320109\2cb60a71-9096-46a5-9793-2167287c4411.jpg" />:</p><sec id="s6_1_1"><title>Dispersion Equation for the Unstable Mode</title><p>The discriminant of this Equation is the same as in the nonviscous case, so the dispersion equation for the unstable mode has the same condition, namely <img src="13-2320109\5c7d15af-7e28-4cbf-83aa-81ce3de51766.jpg" /> <img src="13-2320109\86a013ff-587c-4649-a5b6-ff2483a78963.jpg" />, which leads to:</p><p><img src="13-2320109\5d0f4ed5-3456-4658-b667-88c12a31d943.jpg" /></p><p>where</p><disp-formula id="scirp.41063-formula31631"><label>(101)</label><graphic position="anchor" xlink:href="13-2320109\61de61a5-c559-469a-b242-420f7a9c1197.jpg"  xlink:type="simple"/></disp-formula><p>It is to be noted that the growth rate <img src="13-2320109\9ad22d02-9589-4206-9405-59b4d9a547a5.jpg" /> is maximal for<img src="13-2320109\e2aafca0-af8e-444e-b5cf-89e0beec30fd.jpg" />, which can be considered as the characteristic scale of the generated vortex structures. Below is <xref ref-type="fig" rid="fig3">Figure 3</xref> showing the evolution of <img src="13-2320109\cc74c5d2-6f55-415f-9cf0-5e8cfcbe0ad9.jpg" /> with respect to the wave number <img src="13-2320109\bc1fbd26-385d-4134-ba52-897c92c0f675.jpg" /> for<img src="13-2320109\c4fe21ff-2b70-4313-8500-0f7851d7e455.jpg" />.</p><p>It can be noted that if the discrimant is positive, we get an oscillation with an exponentially decreasing amplitude.</p><p>With increasing amplitude, the instability becomes nonlinear and stabilizes. As a result, nonlinear vortex structures appear. The nonlinear stage of this instability and the results of numerical simulations will be presented in a future paper.</p></sec></sec></sec><sec id="s7"><title>6. Conclusions and Discussion of the Results</title><p>In this paper, we showed that a large scale instability can appear in a rotating stratified fluid which is under the impact of a simple small scale external force (turbulence). The scale of this instability is much larger than the scale of the external force or turbulence. It is important to emphasize that, unlike previous papers about large scale instabilities, in the present paper, there are no special constraints imposed on the external force. It has a zero helicity and its parity needs not be violated; this means that this is a general force. Nevertheless, the small scale turbulence under the impact of the Coriolis force and the buoyancy force becomes helical. This helicity<img src="13-2320109\2b81c3e1-c223-43e1-8022-a9e59718de02.jpg" />, finally, is responsible for the generation of large scale instabilities because the growth rate <img src="13-2320109\e5b7f338-4222-407c-aed9-a62b78ea96ac.jpg" /> is proportional to<img src="13-2320109\e1a96b7c-ec3b-4d78-b32c-1be7bcb8693b.jpg" />. The instability itself is oscillating while its frequency <img src="13-2320109\645b1fa7-f5ed-404b-91df-f4041d046a24.jpg" /> and <img src="13-2320109\c6c9f3b8-5d78-42a6-b2b7-c8a35ea07bec.jpg" /> have, in principle, the same order. This means that the instability in the general case is aperiodic. The frequency of both the stable and unstable oscillations is also proportional to<img src="13-2320109\b04bac90-f41e-4b65-bb4f-ddaa2166e66d.jpg" />. So we can say</p><p>that the oscillation modes are inertial oscillations of the rotating fluid strongly modified by the helicity. There are two oscillating modes: one slow <img src="13-2320109\72b8cecc-8fb3-48c6-8cc5-ec3aa58bccb1.jpg" /> and one fast<img src="13-2320109\4d40bb9c-316f-4bfe-8b63-8f66ec23bc83.jpg" />. These oscillations decay when the viscosity is taken into account and in the case of instability, the maximal growth rate is reached at a characteristic scale of<img src="13-2320109\5f5de56c-8ddb-4a02-86e1-93644aa0d770.jpg" />. Thereby this scale is typical for vortex structures like Beltrami’s runaways. In this paper, the theory of a large scale instability was constructed using the method of multi-scale developments, which was proposed in the work of Frisch, She and Sulem [<xref ref-type="bibr" rid="scirp.41063-ref11">11</xref>]. The nonlinear secular equations for the large scale instability were obtained in the third order of development on a small Reynolds number. In this paper, we studied in detail the linear stage of the instability and the conditions of its appearance. It is interesting to note that instability is possible in the case of both stable and unstable stratifications. Moreover, that neither the Rayleigh number nor the Taylor number are assumed to be either big or small: this means that these numbers are out of scheme parameters. That is the reason why we should state that<img src="13-2320109\f4525cf7-687a-4886-a7d4-33d690264b76.jpg" />, where <img src="13-2320109\177d286c-654a-4950-8c94-1d0ef7cf0200.jpg" /> is the critical Rayleigh number for the generation of convective instability. The unstable stratification is typical for atmosphere dynamics while the stable one is typical for ocean dynamics. We believe that the instability which was found in this paper could be applied to the issue of the generation of large scale vortices in the atmosphere and the ocean, and to some astrophysical problems as well.</p></sec><sec id="s8"><title>REFERENCES</title></sec><sec id="s9"><title>Appendix</title>Calculation of the Reynolds Stress Tensor<p>In order to calculate the Reynolds stress, we begin with the general expression</p><disp-formula id="scirp.41063-formula31632"><label>(102)</label><graphic position="anchor" xlink:href="13-2320109\0863f675-281c-4d6d-9d56-17007e175383.jpg"  xlink:type="simple"/></disp-formula><p>with</p><disp-formula id="scirp.41063-formula31633"><label>(103)</label><graphic position="anchor" xlink:href="13-2320109\4a77b08f-2061-4541-84e8-fd9f058c3272.jpg"  xlink:type="simple"/></disp-formula><p>and</p><disp-formula id="scirp.41063-formula31634"><label>(104)</label><graphic position="anchor" xlink:href="13-2320109\fc20ab6e-2ac8-4b15-acd6-3f132c8f576d.jpg"  xlink:type="simple"/></disp-formula><p>Hence,</p><disp-formula id="scirp.41063-formula31635"><label>(105)</label><graphic position="anchor" xlink:href="13-2320109\5dcff781-cb78-40dc-a3c7-94e840a0e0d5.jpg"  xlink:type="simple"/></disp-formula><p>and <img src="13-2320109\f42f2259-be75-4828-922e-7846d07b716e.jpg" /> has a similar expression.</p><p>Taking into account that only the components <img src="13-2320109\3680843a-d594-40ae-a735-feec100ea445.jpg" /> and <img src="13-2320109\570e6ebc-2332-44bc-9780-c0402cd1cba8.jpg" /> of the external force are nonzero, and after some factorizations, we can write the two contribution of the Reynolds stress tensor in the following form:</p><p><img src="13-2320109\47e0b0e2-52bf-4dfd-8ebc-cef65a4eaef0.jpg" /></p><p>The same calculation for the contribution <img src="13-2320109\7db6282e-99c4-4b64-8fb1-398047ad3464.jpg" /> gives us</p>Calculation of the Helicity<p>The driving force has no helicity, but the joint action of the external force, Coriolis force, and the buoyancy give the internal helicity.</p><p>The general helicity of the velocity field <img src="13-2320109\dded3db3-0496-42e8-96c2-cc4dbcf48081.jpg" /> is expressed by</p><disp-formula id="scirp.41063-formula31636"><label>(106)</label><graphic position="anchor" xlink:href="13-2320109\a82bca3e-88ce-49c9-bcfd-8ace65f1f2d6.jpg"  xlink:type="simple"/></disp-formula><p>where we choose <img src="13-2320109\80bbe2cc-651f-4fb3-9880-d49c33ba73fc.jpg" /> and <img src="13-2320109\c253b97f-462f-4cc7-83ac-b72beec59e10.jpg" /> such that</p><p><img src="13-2320109\2bbc8ed3-743c-41b9-bbef-e6f7d7650511.jpg" /></p><p>and</p><p><img src="13-2320109\47e0b0c6-9cb2-4301-b7c0-2d9b420aa660.jpg" /></p><p>and in indicial notation:</p><p><img src="13-2320109\8c56e8f4-3739-4195-9b9b-796955295376.jpg" /></p><p>We must calculate <img src="13-2320109\50598b2e-81cd-4d59-9138-f5204bbc2d30.jpg" /> with</p><p><img src="13-2320109\ee9342da-5c8e-4d72-9955-cd181a5ed1a4.jpg" /></p><p><img src="13-2320109\82e5ef1f-510a-4069-b8f6-79805f0edfef.jpg" />is calculated in the same way, by replacing <img src="13-2320109\b9f2f450-c77a-4357-b469-1e52e86a69c9.jpg" /> with<img src="13-2320109\a881b21d-addf-4f9b-8e41-e11115bbc6c8.jpg" />.</p><p>We finally obtain</p><p><img src="13-2320109\9eca6d5b-aa73-4e31-93b7-dadf33857aa7.jpg" /></p><p>After linearization:</p><p><img src="13-2320109\23d9889a-5ec9-47c5-ad14-153d0a908331.jpg" /></p><p>where we recall that<img src="13-2320109\ff7c34dc-26b4-4da6-9b7e-d2589f99bfd9.jpg" />.</p><p>One can note that for small perturbations<img src="13-2320109\d2056722-1505-47e4-83de-d58d460a9697.jpg" />, the helicity approaches the constant:</p><p><img src="13-2320109\6417c4a0-5dd1-4e68-bba6-6d352b25629c.jpg" /></p><p>which can be considered as the internal helicity of the field <img src="13-2320109\b3188018-b8e0-4f0a-9853-87b665472fe6.jpg" /> when there are no perturbations.</p></sec></body><back><ref-list><title>References</title><ref id="scirp.41063-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">J. 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