<?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.2013.32009</article-id><article-id pub-id-type="publisher-id">OJFD-32662</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>
 
 
  Non Linear Vortex Structures in Stratified Fluid Driven by Small-Scale Helical Force
 
</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>Vladimir</surname><given-names>Yanovsky</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Institute for Single Cristals, Nat. Academy of Science Ukraine, Kharkov, Ukraine</addr-line></aff><aff id="aff1"><addr-line>Université de Toulouse [UPS], CNRS, Institut de Recherche en Astrophysique et Planétologie,Toulouse Cedex, France</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>anatoly.tour@irap.omp.eu(NT)</email>;<email>yanovsky@isc.kharkov.ua(VY)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>05</day><month>06</month><year>2013</year></pub-date><volume>03</volume><issue>02</issue><fpage>64</fpage><lpage>74</lpage><history><date date-type="received"><day>April</day>	<month>8,</month>	<year>2013</year></date><date date-type="rev-recd"><day>May</day>	<month>8,</month>	<year>2013</year>	</date><date date-type="accepted"><day>May</day>	<month>16,</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><html>
 <head></head>
 
   In this work, we consider the effect of a small-scale helical driving force on fluid with a stable temperature gradient with Reynolds number <img style="border-bottom:0px;border-left:0px;border-top:0px;border-right:0px;" alt="" src="Edit_759e9719-30ed-408d-84a9-809e62187d2b.bmp" />. At first glance, this system does not have any instability. However, we show that a large scale vortex instability appears in the fluid despite its stable stratification. In a non-linear mode this instability becomes saturated and gives a large number of stationary spiral vortex structures. Among these structures there is a stationary helical soliton and a kink of the new type. The theory is built on the rigorous asymptotical method of multi-scale development. 
 
</html></p></abstract><kwd-group><kwd>Vortex Structures; Large Scale Instability; Small Scale Helical Force; AKA-Effect</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The importance of the generation processes of large-scale coherent vortex structures in hydrodynamics is well known. A large-scale vortex means a vortex which is generated by a much smaller scale force or in turbulence with a characteristic scale much smaller than a vortex scale. When these coherent structures appear in smallscale turbulence they play a key role in transfer processes (see for instance [<xref ref-type="bibr" rid="scirp.32662-ref1">1</xref>]). Numerical and laboratory experiments [2-7], confirm the existence of coherent vortex structures, especially for two-dimensional or quasi twodimensional turbulence [7-9]. Notably, they are well observed in geophysical hydrodynamics like various cyclones in the planet’s atmospheres [10,11]. Sometimes the appearance of large scale vortex structures is accompanied by the inverse cascade of energy both in the three-dimensional case (AKA-effect [<xref ref-type="bibr" rid="scirp.32662-ref12">12</xref>]), and in quasitwo-dimensional cases as well [3-6,8,9]. It may be said that the inverse cascade itself is also one of the mechanisms of the generation of large-scale structures [4,13]. The generation of large scale slow movements by small scale external forces in a rotating stratified fluid was also studied numerically in works [14,15]. One of the important large scale instabilities in non compressible fluid is the AKA-effect (Anisotropic Kinetic Alpha effect) which was found in work of Frisch, She and Sulem [<xref ref-type="bibr" rid="scirp.32662-ref16">16</xref>]. In this work a large scale instability appears under the impact of small scale force in which parity is broken (with zero helicity). In the following work [<xref ref-type="bibr" rid="scirp.32662-ref17">17</xref>] the inverse cascade of energy and the non linear mode of instability saturation were studied. Despite the fact that the broken parity is a more general notion than helicity, it is the helicity <img src="6-2320059\a58488a8-ed65-42c8-a085-7c1b75828e43.jpg" /> which is the widespread mechanism of broken parity in hydrodynamical flow. For instance, the turbulence becomes helical when rotation and stratification are taken into account [18-20]. Therefore one may consider the small-scale helical force the parametrization of this turbulence. The injection of a helical external force into hydrodynamic systems was considered in many works ([21-24]), and as a result it was understood that a small-scale turbulence able to generate large-scale perturbations cannot be simply homogeneous, isotropic and helical [<xref ref-type="bibr" rid="scirp.32662-ref25">25</xref>], but must have additional special properties. In some cases the existence of large-scale instability was shown (vortex dynamo or hydrodynamic <img src="6-2320059\dd3fcd1b-b31e-4c00-83a8-bc07b10a06e9.jpg" />-effect). (In the magneto hydrodynamics of conductive fluid the <img src="6-2320059\f74ce366-f0b6-4ed0-bac2-ad1c8dbe21cc.jpg" />-effect is well known [<xref ref-type="bibr" rid="scirp.32662-ref26">26</xref>] ). In particular, in work [<xref ref-type="bibr" rid="scirp.32662-ref22">22</xref>] it is shown that large-scale instability exists in convective systems with small-scale helical turbulence. These works as well as the results of numerical modelling are described in detail in review [<xref ref-type="bibr" rid="scirp.32662-ref27">27</xref>], which are focused essentially on the possible application of these results to the issue of tropical cyclone origination.</p><p>In this work we consider the theory of large scale vortex generation in stratified fluid under the impact of small scale helical force. Let us suppose that there is a stable temperature stratification in fluid. To this fluid with the Reynolds number <img src="6-2320059\fdbe4649-40c1-4ba3-9cab-9d1031b7373d.jpg" /> let us apply a smallscale, helical, external force. This force will maintain in the fluid small-scale helical fluctuations of velocity field <img src="6-2320059\cb5faf27-2743-4239-a109-225dac38aa73.jpg" /> We consider the fluid as being boundless. At first glance there are no instabilities at all in this system. However, we show in this work that despite stable stratification, a large-scale vortex instability appears in the fluid which leads to the generation of large-scale vortex structures. The theory of this instability is built rigourously using the method of asymptotical multi-scale development similar to what was done in work of Frisch, She and Sulem for the theory of AKA-effect [<xref ref-type="bibr" rid="scirp.32662-ref16">16</xref>]. But the equations which we solve differ considerably from equations in work [<xref ref-type="bibr" rid="scirp.32662-ref16">16</xref>]. In addition to linear theory, we also develop and study in details the non-linear theory of this instability saturation. We devote special attention to stationary, non-linear, periodical vortex structures which appear as a result of the saturation of found instability. Among these structures there is a spiral vortex soliton and kink of the new type. In order to distinguish our instability from others in stratified fluid we consider the case of stable stratification. Nevertheless our theory permits the examination of unstable stratification as well by means of substitution <img src="6-2320059\9fb764d6-5cf0-4579-8c27-cce7a12b2819.jpg" /> However, in this case we have to consider that the usual convective instability is eliminated and the Raleigh number is reasonably small.</p><p>Our work is arranged as follows: in Section 2 we set forth the formulation of the problem and equations for stable stratification in Boussinesq approximation; in Section 3 we examine the principal scheme of multi scale development and we give secular equations. In Section 4 we describe external force properties and calculate the Reinolds stress. In Section 5 we discuss the non-linear stage of the instability and its saturation. We study the equations of non-linear instability and its stationary solutions. It is shown that due to the hamiltonian nature of these equations a large number of stationary vortex structures of spiral type appear. We also demonstrate that there are solutions in the form of the spiral soliton and the kink of new type. The obtained results are discussed in the conclusion in Section 6.</p></sec><sec id="s2"><title>2. Main Equations and Formulation of the Problem</title><p>Let us consider the equations for the motion of non compressible fluid with a constant temperature gradient in the Boussinesq approximation:</p><disp-formula id="scirp.32662-formula121368"><label>(1)</label><graphic position="anchor" xlink:href="6-2320059\a365b147-f97b-4f41-a8e5-9fe0447ed9e1.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121369"><label>(2)</label><graphic position="anchor" xlink:href="6-2320059\c88cf95d-1456-4570-ae50-ec6432cd0486.jpg"  xlink:type="simple"/></disp-formula><p><img src="6-2320059\3cc6b463-929e-4f46-8d90-f609ecc3e826.jpg" />—is the unit vector in the direction of axis<img src="6-2320059\5456fb31-5c64-4e0c-af0e-2c1f9e92e392.jpg" />,<img src="6-2320059\c2261129-603c-4b83-bd53-808bddb9c4a6.jpg" />—is the thermal expansion coefficient,</p><p><img src="6-2320059\92706e89-4027-4fae-a21b-5101c3755d97.jpg" />—constant equilibrium gradient of temperature,</p><p><img src="6-2320059\f9797b00-ac8a-420e-8ba3-164d6cbc7ea0.jpg" />. <img src="6-2320059\d22aa6b4-a8a8-4045-9863-6fa452c3456f.jpg" />The buoyancy force and the external force <img src="6-2320059\ccfc1291-e774-4002-afaa-9ebf0f3233d9.jpg" /> <img src="6-2320059\83c4bdf3-29c6-4c7f-8d88-3eab71aef60e.jpg" /> are taken into account in Euler Equation (1). Let us note the force</p><p><img src="6-2320059\ab18934c-51b4-4b34-a71c-703f77331eef.jpg" />in the form:<img src="6-2320059\8e3b5e00-580b-467c-a393-b719f9780d0d.jpg" />, where<img src="6-2320059\5258b97f-fafb-4cb4-b8ec-01c089f5b179.jpg" />—charac teristic scale,<img src="6-2320059\34437e19-035f-41b9-869e-f57835151d45.jpg" />—characteristic time,<img src="6-2320059\57236812-34c9-44ec-af93-0d48ad776333.jpg" />—characteristic amplitude of external force. We designate characteristic velocity, which is engendered by external force as</p><p><img src="6-2320059\e3f07cf0-392a-48a3-8ea7-04870bdaf062.jpg" />. We choose the dimensionless variables</p><p><img src="6-2320059\114cb5ec-34fe-487f-87aa-83a0a4138119.jpg" />:</p><p><img src="6-2320059\28d49361-6bef-481a-9395-02b848cfb40a.jpg" /></p><p>Then:</p><p><img src="6-2320059\d9981152-dded-450e-b7a2-e1a0cad156b4.jpg" /></p><p>where<img src="6-2320059\0b95b84a-e580-4def-8003-6523d26e2127.jpg" />—Reynolds number on the scale<img src="6-2320059\fbeda1b2-c4d8-4723-ae22-91bebe11fecd.jpg" />,<img src="6-2320059\d9300af7-cddb-49cf-8f94-815738d27778.jpg" />—is Prandtl number. We introduce the dimensionless temperature<img src="6-2320059\358e5869-85c8-4dc0-8984-844508e18d25.jpg" />, and obtain the equations system:</p><p><img src="6-2320059\dbe681fc-b38f-4214-afd0-2b50c910a038.jpg" /></p><p>Here<img src="6-2320059\aaf9fa0d-0ce5-4f82-8580-b82d699df269.jpg" />—is Rayleigh number on the scale</p><p><img src="6-2320059\2ca33726-dbdf-4c49-a75f-2457ae5255df.jpg" />. Further for the purpose of simplification we will consider the case<img src="6-2320059\ecf8beca-3378-4c46-9828-9df27bdbfcc3.jpg" />. We pass to the new temperature<img src="6-2320059\c121bfea-354e-41ac-a77a-75a3db21ce5f.jpg" />, and obtain:</p><disp-formula id="scirp.32662-formula121370"><label>(3)</label><graphic position="anchor" xlink:href="6-2320059\97549744-5836-4285-b86d-ef7ff4becb9f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121371"><label>(4)</label><graphic position="anchor" xlink:href="6-2320059\ca66fc5a-2465-4e06-a969-2217e9dc44ac.jpg"  xlink:type="simple"/></disp-formula><p><img src="6-2320059\eea0213a-e96d-428a-a11d-316a418cac3b.jpg" /></p><p>Although we essentially pay attention to stable temperature stratification, unstable stratification can also be considered in the frame of this scheme. We use dimensionless writing of the equation more typically for the problem of convection.</p><p>We will consider as a small parameter of asymptotical development the Reynolds number <img src="6-2320059\7f5bab0a-2ddf-4d27-90dd-fcf4649ea8c8.jpg" /> on the scale<img src="6-2320059\fddf2632-ece0-4108-8359-894d3fea7508.jpg" />. The parameter <img src="6-2320059\90645e09-ecb5-4385-95c6-62fabcb1826e.jpg" /> will be considered neither big nor small, without any impact on development scheme (i.e. outside of the scheme parameters).</p><p>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 non-linear interactions in some orders of perturbation theory, non zero terms can occur after averaging. This means that they are not oscillatory, that is to say large scale. From a formal point of view these terms are secular, i.e. create conditions for the solvability of the large scale asymptotic development. So, to find and study the solvability equations i.e. the equations for large scale perturbations is actually the purpose of this work. Let us designate further the small scale variables as</p><p><img src="6-2320059\d8755be7-2105-4b24-9325-c0b318cfccd3.jpg" />, and large scale ones as<img src="6-2320059\6f16ac69-32f4-4bed-8c93-b86db944e0cc.jpg" />. The derivative <img src="6-2320059\0ed21b8d-cead-42b6-ac60-ecc953bea196.jpg" /> is designated<img src="6-2320059\836e4e58-ac02-49e7-852f-786b85e8b6d8.jpg" />, the derivative <img src="6-2320059\5ebd0e07-9f56-4fd5-a008-173d44a286ee.jpg" /> is designated<img src="6-2320059\915c10c3-75fd-4b58-8fd5-ada014cdde10.jpg" />, and derivatives of large scale variables are <img src="6-2320059\73cdf395-ec19-461b-b029-223766f53178.jpg" /> and <img src="6-2320059\eee016ab-2606-4591-b5d7-fff7025d8f19.jpg" /> respectively (No confusion misunderstanding occurs between the temperature and the large scale time since time is argument and temperature is function). To construct a multi scale asymptotic development we follow the method which is proposed in work [<xref ref-type="bibr" rid="scirp.32662-ref16">16</xref>]. We could start by establishing linear theory for instability development and after that pass to non linear theory, but as the non linear theory is technically less bulky, so we construct the non linear theory directly and then consider the linear limit.</p></sec><sec id="s3"><title>3. The Multi-Scale Asymptotical Development</title><p>Let us search the solution for Equations (3) and (4) in the following form:</p><p><img src="6-2320059\5396046d-e16f-48f9-9fc4-f6e764e89d35.jpg" /> &#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;&#160;(5)<img src="6-2320059\78311203-f422-4fe9-9829-789892c053ac.jpg" />&#160;&#160;&#160;&#160;&#160;&#160;&#160; &#160;(6)</p><disp-formula id="scirp.32662-formula121372"><label>(7)</label><graphic position="anchor" xlink:href="6-2320059\1ed65708-aaa0-4931-8d50-b9babc72ccf9.jpg"  xlink:type="simple"/></disp-formula><p>First of all, we develop space and time derivatives in Equations (3) and (4) into asymptotical series of the form:</p><disp-formula id="scirp.32662-formula121373"><label>(8)</label><graphic position="anchor" xlink:href="6-2320059\11630781-1d97-42ff-9d87-0b69e46f3964.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121374"><label>(9)</label><graphic position="anchor" xlink:href="6-2320059\3bf6ab4b-7690-44a1-bd0f-949b43d4da27.jpg"  xlink:type="simple"/></disp-formula><p>Substituting these expressions into the initial Equations (3) and (4) and gathering together the terms of the same order, we obtain the equations of multi scale asymptotical development and write down the obtained equations up to order <img src="6-2320059\d7a44348-70e0-4410-9d1a-2d9fb6e534ac.jpg" /> inclusive. Let us present the algebraical structure of the asymptotical development of the Equations (3) and (4) for the non linear theory (we will not write indices because they can be restored trivially at any moment). In the order <img src="6-2320059\3f9ad010-4fc5-461f-aaaf-cc49b731bb78.jpg" /> there is only the equation:</p><disp-formula id="scirp.32662-formula121375"><label>(10)</label><graphic position="anchor" xlink:href="6-2320059\8c84a6a2-6fc1-4aad-b26f-76e49dca5626.jpg"  xlink:type="simple"/></disp-formula><p>In the order <img src="6-2320059\c0b5f67b-7d53-481b-ab04-78c2610a9ed4.jpg" /> we have the equation :</p><disp-formula id="scirp.32662-formula121376"><label>(11)</label><graphic position="anchor" xlink:href="6-2320059\f3db95a7-3894-40a3-8a9d-f309a55d035d.jpg"  xlink:type="simple"/></disp-formula><p>In the order <img src="6-2320059\c68d6c2f-29cc-4408-b9c9-a2bac0c94c8e.jpg" /> we get a system of equations:</p><disp-formula id="scirp.32662-formula121377"><label>(12)</label><graphic position="anchor" xlink:href="6-2320059\614485ed-b99c-4979-be19-85bc2af77ae7.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121378"><label>(13)</label><graphic position="anchor" xlink:href="6-2320059\5bf278f0-cb1a-4f6b-8a4c-abe29d7f4af4.jpg"  xlink:type="simple"/></disp-formula><p><img src="6-2320059\3f716026-fba2-4f08-8aa2-fbcab56eea02.jpg" /></p><p>The system of Equations (12) and (13) gives secular terms:</p><disp-formula id="scirp.32662-formula121379"><label>(14)</label><graphic position="anchor" xlink:href="6-2320059\563f404d-257f-440f-9a25-d38a1112362b.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121380"><label>(15)</label><graphic position="anchor" xlink:href="6-2320059\74d8e443-752a-48f8-b6d0-d94a879e1543.jpg"  xlink:type="simple"/></disp-formula><p>In zero order <img src="6-2320059\2a3c19e0-7d3f-4e98-92dd-58e0142f3825.jpg" /> we have the following system of equations:</p><disp-formula id="scirp.32662-formula121381"><label>(16)</label><graphic position="anchor" xlink:href="6-2320059\42cd2dae-24c2-4f23-b1b8-e9c3f5829a98.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121382"><label>(17)</label><graphic position="anchor" xlink:href="6-2320059\24f339f1-34f7-4d7a-b686-28baaa437075.jpg"  xlink:type="simple"/></disp-formula><p><img src="6-2320059\ae888f35-d9bf-4825-b995-ed586040967a.jpg" /></p><p>These equations give one secular equation:</p><disp-formula id="scirp.32662-formula121383"><label>(18)</label><graphic position="anchor" xlink:href="6-2320059\4feeade6-ccd4-4d9d-8e16-4653f2b7911c.jpg"  xlink:type="simple"/></disp-formula><p>Consider the equations of the first approximation R:</p><disp-formula id="scirp.32662-formula121384"><label>(19)</label><graphic position="anchor" xlink:href="6-2320059\697599e0-8b90-4973-ac8d-453f22482b05.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121385"><label>(20)</label><graphic position="anchor" xlink:href="6-2320059\c9edad12-bfc6-445d-9776-2e0c70332116.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121386"><label>(21)</label><graphic position="anchor" xlink:href="6-2320059\b213d306-2b56-42af-a1c9-0dacb3ec9c5d.jpg"  xlink:type="simple"/></disp-formula><p>From this system of equations follow the secular equations:</p><disp-formula id="scirp.32662-formula121387"><label>(22)</label><graphic position="anchor" xlink:href="6-2320059\62b1c454-f6b7-4e77-906b-e6004b47b1ee.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121388"><label>(23)</label><graphic position="anchor" xlink:href="6-2320059\122e7cac-569c-4b19-a59f-8ac22c27cba5.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121389"><label>(24)</label><graphic position="anchor" xlink:href="6-2320059\79ea019c-d46b-46eb-a7bf-8ef92bf5dbe1.jpg"  xlink:type="simple"/></disp-formula><p>The secular Equations (22)-(24), are clearly obviously satisfied for velocity field geometry:</p><disp-formula id="scirp.32662-formula121390"><label>(25)</label><graphic position="anchor" xlink:href="6-2320059\c8c52936-a585-445d-a5c9-098384f362c6.jpg"  xlink:type="simple"/></disp-formula><p>In the second order<img src="6-2320059\7f02e546-28fe-413b-a93b-791dcc397f94.jpg" />, we obtain equations:</p><disp-formula id="scirp.32662-formula121391"><label>(26)</label><graphic position="anchor" xlink:href="6-2320059\eab13fa4-31fc-4bc1-82c1-07b44f7b3cc7.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121392"><label>(27)</label><graphic position="anchor" xlink:href="6-2320059\b9afde8f-502d-4c97-8806-45beeda29084.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121393"><label>(28)</label><graphic position="anchor" xlink:href="6-2320059\339bf245-33e3-40e2-b519-5386ef98e253.jpg"  xlink:type="simple"/></disp-formula><p>It is easy to see that in the order <img src="6-2320059\683902f0-8dde-418e-a3fc-10c064368b8c.jpg" /> there are no secular terms.</p><p>Let us come now to the most important order<img src="6-2320059\314448b8-0f6e-4e4a-9c36-d9a2e2800029.jpg" />. In this order we obtain equations:</p><disp-formula id="scirp.32662-formula121394"><label>(29)</label><graphic position="anchor" xlink:href="6-2320059\823aaf1c-a9a1-446b-bc59-023a4d8bdae6.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121395"><label>(30)</label><graphic position="anchor" xlink:href="6-2320059\0f88af57-5a25-4734-adf0-91b360aa1c9e.jpg"  xlink:type="simple"/></disp-formula><p>From this we get the main secular equation:</p><disp-formula id="scirp.32662-formula121396"><label>(31)</label><graphic position="anchor" xlink:href="6-2320059\272367ad-fb32-4ff3-8918-d892a5016609.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121397"><label>(32)</label><graphic position="anchor" xlink:href="6-2320059\7c8d556f-97f0-4433-a31f-a6dc3fd69ed6.jpg"  xlink:type="simple"/></disp-formula><p>In these equations we do not write the law index<img src="6-2320059\137fe615-c15e-4268-9871-f15c7e7547d5.jpg" />. Besides there are secular equations:</p><disp-formula id="scirp.32662-formula121398"><label>(33)</label><graphic position="anchor" xlink:href="6-2320059\266e793c-63ca-4526-95d6-6d1506ff0374.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121399"><label>(34)</label><graphic position="anchor" xlink:href="6-2320059\e2db2cda-25d2-4a1f-ba00-4bdc6060b373.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121400"><label>(35)</label><graphic position="anchor" xlink:href="6-2320059\b77e4bf1-4c0e-478c-9819-beb327fc38a3.jpg"  xlink:type="simple"/></disp-formula><p>The Equations (33)-(35) are satisfied in the previous geometry:</p><disp-formula id="scirp.32662-formula121401"><label>(36)</label><graphic position="anchor" xlink:href="6-2320059\2ec24653-57b4-4749-bd77-5ab905591e6b.jpg"  xlink:type="simple"/></disp-formula><p>There is also an equation to find the pressure<img src="6-2320059\7c5d7407-b449-4114-90d5-5d24fefe43a1.jpg" />:</p><disp-formula id="scirp.32662-formula121402"><label>(37)</label><graphic position="anchor" xlink:href="6-2320059\bd30497f-3600-4634-ae24-7b02bf4e0ba7.jpg"  xlink:type="simple"/></disp-formula><p>These formulae show that when one knows the velocity it is possible to restore temperature and pressure.</p></sec><sec id="s4"><title>4. Calculations of the Reynolds Stresses</title><p>It is clear that the essential equation for finding the non linear alpha-effect is Equation (31). In order to obtain these equations in the closed form we need to calculate the Reynolds stresses<img src="6-2320059\6b9e30c8-c306-4c4e-94ab-1573a9e3f324.jpg" />. First of all we have to calculate the fields of zero approximation <img src="6-2320059\b6770254-efed-4852-bb2c-870f77543225.jpg" /> from the asymptotical development in zero order we have the equations:</p><disp-formula id="scirp.32662-formula121403"><label>(38)</label><graphic position="anchor" xlink:href="6-2320059\6b0aac4f-e544-4fce-8f54-f3971c609cd5.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121404"><label>(39)</label><graphic position="anchor" xlink:href="6-2320059\7700fab5-950e-4fb7-b83a-8eb5f541e1dd.jpg"  xlink:type="simple"/></disp-formula><p>Let us introduce the operator<img src="6-2320059\1624fa61-74bd-49c5-9d79-b222c47a69c4.jpg" />:</p><disp-formula id="scirp.32662-formula121405"><label>(40)</label><graphic position="anchor" xlink:href="6-2320059\6add35bb-919a-407b-8fd7-23ed991dfe5b.jpg"  xlink:type="simple"/></disp-formula><p>Using the operator<img src="6-2320059\3d6b98fd-144b-4a8c-abc9-11e4b42c2f67.jpg" />, we write down Equations (38) and (39) in the form:</p><disp-formula id="scirp.32662-formula121406"><label>(41)</label><graphic position="anchor" xlink:href="6-2320059\29a7fe04-89f5-40df-96c8-c6693373dcf7.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121407"><label>(42)</label><graphic position="anchor" xlink:href="6-2320059\23fa157c-5b75-4c96-92d3-7362251d171d.jpg"  xlink:type="simple"/></disp-formula><p>Eliminating the temperature and pressure from Equation (41) we obtain:</p><disp-formula id="scirp.32662-formula121408"><label>(43)</label><graphic position="anchor" xlink:href="6-2320059\5544d48c-ab8d-4595-a6be-36ecb547f192.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="6-2320059\de4e7be4-d1dd-452e-b001-155da8e5e56c.jpg" /> is the projection operator:</p><p><img src="6-2320059\cc1c7be7-e08c-4af1-af01-3fe11c6c2f7a.jpg" /></p><p>Dividing this equation by<img src="6-2320059\108ad45f-950d-40b3-9291-0bca18576e84.jpg" />, we can write it in the form:</p><disp-formula id="scirp.32662-formula121409"><label>(44)</label><graphic position="anchor" xlink:href="6-2320059\57c7fe46-9a65-4501-8976-7c86ead864fa.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="6-2320059\3811aea0-0ce7-46e5-baf8-e2393a6c9e54.jpg" /> is the operator:</p><disp-formula id="scirp.32662-formula121410"><label>(45)</label><graphic position="anchor" xlink:href="6-2320059\12373180-85d5-4ee4-bc54-19870f17d0e7.jpg"  xlink:type="simple"/></disp-formula><p>It is easy to make sure by a direct check that the inverse operator <img src="6-2320059\1c75623c-fc01-49a7-9b95-59b221ae9ba8.jpg" /> has the form:</p><disp-formula id="scirp.32662-formula121411"><label>(46)</label><graphic position="anchor" xlink:href="6-2320059\7b17780c-ccb6-41da-9952-2e360068de1a.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121412"><label>(47)</label><graphic position="anchor" xlink:href="6-2320059\8a86f3b3-a14f-4b7c-a192-93a702e6fb24.jpg"  xlink:type="simple"/></disp-formula><p>Consequently the expression for the velocity and temperature<img src="6-2320059\07b05d2a-3173-4126-8d64-b6b74e8f8e54.jpg" />, <img src="6-2320059\f7423320-f3de-4314-bcfd-837f8224ee70.jpg" />takes the form:</p><disp-formula id="scirp.32662-formula121413"><label>(48)</label><graphic position="anchor" xlink:href="6-2320059\bde26299-8a12-45f4-8765-a960201e13a3.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121414"><label>(49)</label><graphic position="anchor" xlink:href="6-2320059\20dd8aba-d8e6-42ce-baf2-41d21efd691e.jpg"  xlink:type="simple"/></disp-formula><p>In order to use these formulae we have to specify in explicit form the helical external force<img src="6-2320059\a44a8b4e-87eb-4f33-ba95-b3bc7a71cdec.jpg" />. The most simple and natural way is to specify the external force as deterministic. (Certainly, it is possible to specify the external force in a statistical way with specifying random field correlators, but this leads to more bulky calculations). As it is known helicity means that<img src="6-2320059\1f99031c-b1ff-44ef-8e60-94eccf5d924b.jpg" />. Let us specify the force <img src="6-2320059\d6a9ffb6-28f3-4b5f-b90e-946c5fde9199.jpg" /> like so:</p><disp-formula id="scirp.32662-formula121415"><label>(50)</label><graphic position="anchor" xlink:href="6-2320059\a1a2458b-662a-443e-a617-d4360052cc9a.jpg"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.32662-formula121416"><label>(51)</label><graphic position="anchor" xlink:href="6-2320059\da82e914-5fa9-400f-a9ba-37e633ce1f44.jpg"  xlink:type="simple"/></disp-formula><p>or</p><disp-formula id="scirp.32662-formula121417"><label>(52)</label><graphic position="anchor" xlink:href="6-2320059\fd367ba6-6448-4d01-b93b-4016553a7c4e.jpg"  xlink:type="simple"/></disp-formula><p>It is evident that<img src="6-2320059\21a9d4c0-ebbe-4746-b548-4c2aea82844c.jpg" />, where<img src="6-2320059\3bfec757-8be7-4e6d-bce6-2cf437246927.jpg" />—is the single pseudo scalar, i.e. helicity is equal to:</p><disp-formula id="scirp.32662-formula121418"><label>(53)</label><graphic position="anchor" xlink:href="6-2320059\a3c91410-6ea1-403a-a0e9-0813263bec1f.jpg"  xlink:type="simple"/></disp-formula><p>The formulae (50) and (52) allow us to easily make intermediate calculations, but in the final formulae we obviously shall take <img src="6-2320059\fb6ef52d-320a-420d-8bce-73ec1fa45274.jpg" /> as equal to one, since external force is dimensionless and depends only on dimensionless space and time arguments. The force (50) is physically simple and can be realized in laboratory experiments and in numerical simulation.</p><p>It is easy to write down the force (50) in complex form. It is evident that:</p><disp-formula id="scirp.32662-formula121419"><label>(54)</label><graphic position="anchor" xlink:href="6-2320059\f6f3cb67-8ccc-4915-9542-0127b1503a65.jpg"  xlink:type="simple"/></disp-formula><p>where vectors <img src="6-2320059\05053e04-d2d6-4be5-a510-174d33c442d5.jpg" /> and <img src="6-2320059\c8d4b3c5-e94a-40d4-8ee7-a7588d2e5d28.jpg" /> has the form:</p><disp-formula id="scirp.32662-formula121420"><label>(55)</label><graphic position="anchor" xlink:href="6-2320059\d4fe0ddd-162f-4dfb-8166-534865242319.jpg"  xlink:type="simple"/></disp-formula><p>and <img src="6-2320059\d4792eb5-14d4-4a6d-861f-9162259b30a9.jpg" /> are given by formulae (52). The effect of the operator <img src="6-2320059\55266fd3-9c38-4033-a6b0-b4445895190d.jpg" /> on proper function <img src="6-2320059\60662c26-5359-4357-ba87-a0a8d833eb35.jpg" /> has obviously the form:</p><p><img src="6-2320059\b64ef869-6641-4690-9bdc-13cc6cdff10b.jpg" />, where</p><p><img src="6-2320059\06231372-3b52-4516-9961-6562899b3097.jpg" />is:</p><disp-formula id="scirp.32662-formula121421"><label>(56)</label><graphic position="anchor" xlink:href="6-2320059\4a075f38-1e71-4fa9-b6c8-11b2455aa1fd.jpg"  xlink:type="simple"/></disp-formula><p>From this it is evident that:</p><disp-formula id="scirp.32662-formula121422"><label>(57)</label><graphic position="anchor" xlink:href="6-2320059\36ca4923-4cbe-438f-a060-ee021cd78cbb.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121423"><label>(58)</label><graphic position="anchor" xlink:href="6-2320059\50937b08-1ec0-4dc7-9959-b99c5bd78225.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121424"><label>(59)</label><graphic position="anchor" xlink:href="6-2320059\94774456-6466-4d00-b02d-829eefb4f171.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121425"><label>(60)</label><graphic position="anchor" xlink:href="6-2320059\be6e6407-9655-480a-9970-da11c56559dd.jpg"  xlink:type="simple"/></disp-formula><p>From the formulae (48) and (54), follows that the field <img src="6-2320059\49e33587-647d-4496-9b5d-15ee57b30d2b.jpg" /> is composed of four terms: <img src="6-2320059\b4854949-6b4e-4854-9182-a99e73819ad8.jpg" />where</p><disp-formula id="scirp.32662-formula121426"><label>(61)</label><graphic position="anchor" xlink:href="6-2320059\3444aea0-f35c-4ee2-9e53-0a956969a499.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121427"><label>(62)</label><graphic position="anchor" xlink:href="6-2320059\b72b0362-63b3-42a2-b9b1-b7b7671b25f1.jpg"  xlink:type="simple"/></disp-formula><p>As was stated earlier, in scalar operators <img src="6-2320059\332365ec-5eaa-4b97-b7ad-20736d9b2479.jpg" /> one can take<img src="6-2320059\c8bde415-6446-4346-bd3b-be99b8f5f7b3.jpg" />. Then taking into account that<img src="6-2320059\00ae3b4c-6a09-494c-bc6c-05c59b250671.jpg" />, we obtain:</p><disp-formula id="scirp.32662-formula121428"><label>(63)</label><graphic position="anchor" xlink:href="6-2320059\b85b433b-b37c-4d21-8546-2c7b4c5b3e14.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121429"><label>(64)</label><graphic position="anchor" xlink:href="6-2320059\6e346920-aff0-4fce-a4dd-c5be0b23665d.jpg"  xlink:type="simple"/></disp-formula><p>Here we introduced the following notations: <img src="6-2320059\2bd9acb3-2dd3-48e0-a26c-7ee784ce445f.jpg" />. Taking into consideration these formulae we can write down the velocities <img src="6-2320059\1628e38e-1a7c-454a-b9f4-19800b4068ed.jpg" /> in the form:</p><disp-formula id="scirp.32662-formula121430"><label>(65)</label><graphic position="anchor" xlink:href="6-2320059\5105a550-c74e-4720-b28e-f485e7c5f259.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121431"><label>(66)</label><graphic position="anchor" xlink:href="6-2320059\1e167e94-d83b-41b9-bb77-8eab2e06723b.jpg"  xlink:type="simple"/></disp-formula><p>In order to calculate the Reynolds stresses we have first of all to calculate the expression:</p><disp-formula id="scirp.32662-formula121432"><label>(67)</label><graphic position="anchor" xlink:href="6-2320059\7fc61e53-513e-4b1c-a67d-1bcf8f7220e0.jpg"  xlink:type="simple"/></disp-formula><p>Taking into account the formula (65), we obtain:</p><disp-formula id="scirp.32662-formula121433"><label>(68)</label><graphic position="anchor" xlink:href="6-2320059\b133988b-19a0-442b-8650-711e87fb15c4.jpg"  xlink:type="simple"/></disp-formula><p>Similarly taking into account formula (66), we obtain:</p><disp-formula id="scirp.32662-formula121434"><label>(69)</label><graphic position="anchor" xlink:href="6-2320059\71950075-ad5d-4bc3-86d7-32517df4156f.jpg"  xlink:type="simple"/></disp-formula><p>It is clear that the components <img src="6-2320059\40f2ca51-8423-4b6d-8160-3949c39a2ea9.jpg" /> and <img src="6-2320059\dc8f88a1-f584-4ff7-86ac-56fc3f38ce3a.jpg" /> are of interest. To begin with we consider the components of the tensor<img src="6-2320059\8c91155b-589d-4027-93c9-560ce6615eb0.jpg" />.</p><disp-formula id="scirp.32662-formula121435"><label>(70)</label><graphic position="anchor" xlink:href="6-2320059\5170f0b4-f45f-4d48-8057-9e47eb9f851a.jpg"  xlink:type="simple"/></disp-formula><p>since<img src="6-2320059\4db8dcd5-3c26-4c45-ac8f-1a26aae22817.jpg" />.</p><disp-formula id="scirp.32662-formula121436"><label>(71)</label><graphic position="anchor" xlink:href="6-2320059\086ec18f-791f-43a8-9a09-7da54320c5f7.jpg"  xlink:type="simple"/></disp-formula><p>The first bracket in the (71) is equal to zero, which is why:</p><disp-formula id="scirp.32662-formula121437"><label>(72)</label><graphic position="anchor" xlink:href="6-2320059\518f1da6-daef-4964-a2fa-2d31f26df04a.jpg"  xlink:type="simple"/></disp-formula><p>Now consider the component<img src="6-2320059\27c5ffea-8207-4d8c-b213-5193c0a1e647.jpg" />:</p><disp-formula id="scirp.32662-formula121438"><label>(73)</label><graphic position="anchor" xlink:href="6-2320059\6864b3a4-925f-4d8e-b924-d8863aace2fd.jpg"  xlink:type="simple"/></disp-formula><p>as far as<img src="6-2320059\f966e857-874c-4564-bf31-7644887ac4fc.jpg" />. Consider now the component<img src="6-2320059\a1588a7b-256f-49c9-baef-016fc97b9729.jpg" />:</p><disp-formula id="scirp.32662-formula121439"><label>(74)</label><graphic position="anchor" xlink:href="6-2320059\1e2f3e24-02d9-4662-a352-a92464d2b5a7.jpg"  xlink:type="simple"/></disp-formula><p>The first bracket in the formula (74) is equal to zero, then:</p><disp-formula id="scirp.32662-formula121440"><label>(75)</label><graphic position="anchor" xlink:href="6-2320059\466edbf1-0615-433c-a082-bcd81285faf5.jpg"  xlink:type="simple"/></disp-formula><p>Taking into account:</p><disp-formula id="scirp.32662-formula121441"><label>(76)</label><graphic position="anchor" xlink:href="6-2320059\14e38927-d097-4b7a-8b94-9e93d35d3573.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121442"><label>(77)</label><graphic position="anchor" xlink:href="6-2320059\c842a4a2-a64c-470c-98b8-44749d757588.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121443"><label>(78)</label><graphic position="anchor" xlink:href="6-2320059\94cc75c5-a988-477b-90e1-372129e57ed0.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121444"><label>(79)</label><graphic position="anchor" xlink:href="6-2320059\ded643e0-abc8-4bab-978c-a30f9f2db49a.jpg"  xlink:type="simple"/></disp-formula><p>The components <img src="6-2320059\094119bc-df41-495c-bbcc-6f4f265c33ae.jpg" /> take the form:</p><disp-formula id="scirp.32662-formula121445"><label>(80)</label><graphic position="anchor" xlink:href="6-2320059\1a03271e-f1e6-456f-b87a-4c2538be4940.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121446"><label>(81)</label><graphic position="anchor" xlink:href="6-2320059\87fd41dc-f454-43fa-ba20-bf4b30592f98.jpg"  xlink:type="simple"/></disp-formula><p>Now, when we have these tensors components, we can obtain closed equations for velocity.</p></sec><sec id="s5"><title>5. Large-Scale Instability and Non Linear Vortex Structures</title><p>Let us write down in the explicit form the equations for non linear instability:</p><p><img src="6-2320059\cbdb1b50-d637-4d75-bd1c-a317c0f7124b.jpg" /></p><p>(82)</p><p><img src="6-2320059\36bfafda-2b1b-40c7-82bd-1ced3252fdab.jpg" /></p><p>(83)</p><p>It is easy to see that with small values of the variables <img src="6-2320059\38de9a7f-720c-4424-b8f6-765eb8b0ecb4.jpg" /> the Equations (82) and (83) are reduced to linear equations and describe the linear stage of instability.</p><disp-formula id="scirp.32662-formula121447"><label>(84)</label><graphic position="anchor" xlink:href="6-2320059\f44928a9-db8e-4907-8960-858d0b5b7551.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121448"><label>(85)</label><graphic position="anchor" xlink:href="6-2320059\e3124706-1e8f-4d98-957d-d73a1ce5c485.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121449"><label>(86)</label><graphic position="anchor" xlink:href="6-2320059\73aa9ec9-469c-4867-a0e6-b0661154b5bc.jpg"  xlink:type="simple"/></disp-formula><p>Here <img src="6-2320059\af0e3fd1-7c8c-484f-9ab6-ad33e6093d83.jpg" /> designates the single pseudo scalar because expressions <img src="6-2320059\57dd1a5b-5756-478e-8e3d-a595e384465a.jpg" /> are components of<img src="6-2320059\563bd9e2-4856-4af3-bdd8-bb33b035a53d.jpg" />. The Equations (84) and (85) differ from equation of AKA-effect [<xref ref-type="bibr" rid="scirp.32662-ref16">16</xref>] by the coefficient <img src="6-2320059\eab3ff8a-a137-4c51-b182-398ccf34fe76.jpg" /> only, but the important difference between our equations and equations of AKA-effect is the presence of the Rayleigh number in <img src="6-2320059\98c834ee-0136-42da-bae8-55595fc5c5f4.jpg" /> coefficient. As a result: <img src="6-2320059\3a558d1b-54fc-4f6c-9e4c-41fe53228c50.jpg" />in the non stratified fluid. The Equations (84) and (85) obviously contain an instability which generates large scale vortex structures. Choosing the velocities <img src="6-2320059\1f2db4b5-be94-446a-af77-4219f4d4ba4e.jpg" /> in the form:</p><disp-formula id="scirp.32662-formula121450"><label>(87)</label><graphic position="anchor" xlink:href="6-2320059\8971669d-a4e8-46fd-bb82-cbc51b39ad8f.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121451"><label>(88)</label><graphic position="anchor" xlink:href="6-2320059\6465dc16-2e04-4380-8a16-1dbc8af8d0bc.jpg"  xlink:type="simple"/></disp-formula><p>we obtain the instability increment <img src="6-2320059\c5c38be1-7a28-47d3-a69d-89f7694896df.jpg" />i.e..</p><p><img src="6-2320059\b5dd17ee-4e24-469e-870b-bf4646b7dc93.jpg" />with the <img src="6-2320059\a88d8581-df95-49b2-bccd-a219a1b5cf80.jpg" /> The formulae (87) and</p><p>(88) describe a spiral vortex structure (circularly polarized plane wave) with an amplitude which increases exponentially with time. These waves are sometimes called Beltrami runaways since for them there is no usual hydrodynamical interaction<img src="6-2320059\d189b390-081e-4b26-8074-14a79ea63d5d.jpg" />. With <img src="6-2320059\8d53ab51-1375-4037-896a-baf4f7958fef.jpg" /> the linear instability vanishes but the non linear remains.</p><p>If the external force has a zero helicity, then the <img src="6-2320059\e7881a16-057f-43c4-984f-3f97459292de.jpg" />-term vanishes in accordance with the general theorem of Reynolds stress tensor [<xref ref-type="bibr" rid="scirp.32662-ref25">25</xref>]. Helicity is taken into account in the external force structure itself. If the temperature gradient vanishes, then it is evident that the <img src="6-2320059\2976517e-2cca-46b0-8eba-66f836af2fd2.jpg" />-term also vanishes.</p><p>It is clear that with the increasing <img src="6-2320059\e7082050-d86f-4a0c-98f2-ab256d80510b.jpg" /> of the non linear terms decrease and the instability becomes saturated. As a result of the development and stabilization of instability, non linear vortex helical structures appear. The study of the form of these stationary structures is of interest. For that purpose we take (82), (83) <img src="6-2320059\16de438a-029d-41c0-99be-54f1f9fb7fcb.jpg" />. Integrating these equations over<img src="6-2320059\bd59a046-8ae9-4931-bf50-929b00f193a5.jpg" />, we obtain:</p><disp-formula id="scirp.32662-formula121452"><label>(89)</label><graphic position="anchor" xlink:href="6-2320059\e74aada6-c552-466e-a13e-82261901c16e.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32662-formula121453"><label>(90)</label><graphic position="anchor" xlink:href="6-2320059\47dba560-7cb3-4774-a392-d7b0fe7b6e68.jpg"  xlink:type="simple"/></disp-formula><p>Here new variables are introduced <img src="6-2320059\3e9d0c4d-f6fa-4fbb-ae59-b471efeb0767.jpg" />—are integration constants. The system of Equations (89) and (90) can be write down in the hamiltonian form:</p><disp-formula id="scirp.32662-formula121454"><label>(91)</label><graphic position="anchor" xlink:href="6-2320059\32514729-24a8-49ac-9820-6857b02c5ddc.jpg"  xlink:type="simple"/></disp-formula><p>Here the variable <img src="6-2320059\f7a79fb0-0fce-4578-ae6f-a044b9f8e86a.jpg" /> plays the role of time and the hamiltonian <img src="6-2320059\563c3ef1-8766-464c-8d99-b19c1f632f13.jpg" /> has the form:</p><disp-formula id="scirp.32662-formula121455"><label>(92)</label><graphic position="anchor" xlink:href="6-2320059\869b9548-8e54-4a8e-8e25-f7120234a133.jpg"  xlink:type="simple"/></disp-formula><p>where function <img src="6-2320059\849d4c97-309b-46e7-83e3-31e6bce0f8d3.jpg" /> has the form:</p><disp-formula id="scirp.32662-formula121456"><label>(93)</label><graphic position="anchor" xlink:href="6-2320059\72d36b27-f50b-43b1-a0c0-cd8d68863995.jpg"  xlink:type="simple"/></disp-formula><p>The function <img src="6-2320059\1b20ff17-4aec-4fd8-ab13-9ec8e104569b.jpg" /> (92), (93) is obviously the first integral of the equations system (89), (90) and can be found by the direct integration of this system. With <img src="6-2320059\0993ad7a-7257-45d0-8c34-2999745fd37c.jpg" /> the function <img src="6-2320059\365a7e22-86ae-4fc6-b3b2-7bb373061052.jpg" /> is limited above and below as well. That is why the section of this hamiltonian by the constant<img src="6-2320059\2c705ee7-0c95-4f8e-9cb5-6cfb402654e7.jpg" />, gives closed periodical trajectories on the phase plane<img src="6-2320059\0c0483b0-9793-4327-a22f-464b30d9841e.jpg" />, which correspond to the helical vortex structures in real space. Examples of phase pictures for <img src="6-2320059\3ea71f03-38a5-475d-ae35-9c388c90dfc9.jpg" /> and <img src="6-2320059\2e37753a-73aa-4e43-9a41-9b711fb22eb8.jpg" /> are presented in Figures 1 and 2. (As was already mentioned with <img src="6-2320059\8f17e9ec-5f9d-4135-9b15-419c19b78edd.jpg" /> the instability is essentially non linear). With <img src="6-2320059\ff95331d-b625-4fa4-8a90-dcbede5df5ff.jpg" /> there is only one elliptical point on the phase plane. Closed trajectories correspond to the periodical non linear vortex structures. Despite the fact that</p><p>we are mostly interested in a boundless problem, it should be noted that thick closed lines correspond to the non linear structures which are also the solutions of the boundary problem with a rigid boundary:</p><p><img src="6-2320059\a3032ad3-6e9b-45f8-b494-f630439efb38.jpg" /></p><p>where <img src="6-2320059\dadbf303-05b7-4680-8a46-d41ded2c6c03.jpg" /> is the period over <img src="6-2320059\b9558d62-e040-4848-8f3a-915925f2a258.jpg" /> phase trajectory, which gets out with<img src="6-2320059\af61abda-5b64-4e16-a00e-1d0d4b2efedc.jpg" />, from point <img src="6-2320059\ab9fd76c-e1f2-4f74-bdca-6e1c45553d11.jpg" /> and gets back to the same point with <img src="6-2320059\22236586-8a6a-426d-a42f-73c92798d9e9.jpg" /> The space structures of periodical solutions are presented in Figures 3-5. If one of the constants, for instance<img src="6-2320059\bd6e01b7-4de0-4411-b52c-cd2036d4f4ef.jpg" />, then one hyperbolic point appears on phase picture. For instance, phase pictures with <img src="6-2320059\346cf655-0e8b-4bf0-88de-3581a3bb7a5e.jpg" /> are presented in <xref ref-type="fig" rid="fig6">Figure 6</xref>. An example of a periodical nonlinear vortex structure which corresponds to the closed trajectory on a phase plane with<img src="6-2320059\8efaf9fc-3fb1-4a4e-92a6-55a91cd998ca.jpg" />, is given in <xref ref-type="fig" rid="fig7">Figure 7</xref>. In this case the linear instability is obviously absent. The solution which corresponds to the separatrix on <xref ref-type="fig" rid="fig6">Figure 6</xref>. is of particular interest. This solution describes the solitary spiral turn of the velocity field around the axe <img src="6-2320059\63ff73a0-be70-4402-8684-809f77ca9c55.jpg" /> (soliton): see <xref ref-type="fig" rid="fig8">Figure 8</xref>. Moving away from the soliton the velocity field becomes constant. This kind of soliton was not known earlier. The interesting particularity of this soliton is the fact that it is also the solution for the boundary problem with free boundaries. For this boundary problem [<xref ref-type="bibr" rid="scirp.32662-ref28">28</xref>]:</p><p><img src="6-2320059\74513007-6861-4e72-b815-6c4b82d92279.jpg" /></p><p>on the fluid boundary. In addition, boundaries must be at a great distance from soliton, much bigger than the soliton’s characteristic dimensions. In this case at great distances from soliton:<img src="6-2320059\2207aedd-0fcb-44e8-bb9d-b57b7c951793.jpg" />. In a case when there are two constants <img src="6-2320059\2801f1dd-a421-4e06-ab50-5c12a1e09d26.jpg" /> two hyperbolic and two elliptical points appear on the phase picture. The example of this phase picture with C<sub>1</sub> = 0.1,</p><p>C<sub>2</sub> = 0.1 is shown in <xref ref-type="fig" rid="fig9">Figure 9</xref>. As above, the periodic vortex structures correspond to closed trajectories around elliptical points. Localized solutions (solitons) correspond to the separatrix on <xref ref-type="fig" rid="fig9">Figure 9</xref>. Since the separatrix connects two different hyperbolic points the soliton has now two different limiting values, with<img src="6-2320059\9e7dbb5d-80cf-4f27-ac50-95ee8e0b278b.jpg" />, <xref ref-type="fig" rid="fig10">Figure 10</xref>. This soliton is called a kink. Therefore, spiral kinks correspond to the separatrix in <xref ref-type="fig" rid="fig9">Figure 9</xref>. These kinks are</p><p>also solutions for the boundary problem with free boundaries. Thereby in the hamiltonian scheme which we consider there are three kinds of solutions: periodical waves, solitons and solutions moving to infinity. The last ones are not of interest from the point of view of the problem of large cale instability stabilization. In conclusion it should be remembered that the system of the</p><p>Equations (82), (83) is closed. The velocity field <img src="6-2320059\eb857cda-b69e-472f-97d7-a993ad3264b9.jpg" /> determines the pressure <img src="6-2320059\1408ba8e-299a-4d45-9997-b810ccc05e27.jpg" /> and contributes to the equation for temperature (32). Closure of this equation is made in much the same way as closure for velocity. Nevertheless this equation is secondary and here we do not give the result of this closure.</p></sec><sec id="s6"><title>6. Conclusions and Discussion of Results</title><p>In this work it is shown that in fluid with stable stratification a large scale instability appears under the action of small scale helical force. The result of the instability is the generation of vortex structures of the Beltrami type. These vortices have the characteristic vertical dimension <img src="6-2320059\e0eff5f0-571b-4d0a-8ac7-7c83f2dcd185.jpg" /> and a horizontal dimension much bigger than the vertical one. Since the vertical component of the velocity <img src="6-2320059\5e5d7d56-d4da-48ee-b80b-906ea384ce80.jpg" /> is equal to zero in the main approximation and the stratification is stable, then the found instability does not have any relation to convection. The structure of the equation which describes the instability in linear approximation is the same as the equation of <img src="6-2320059\091457a7-5083-4262-968e-b171b5dcbd13.jpg" />-effect or more precisely as the equation of AKA-effect. But as opposed to the AKA-effect, <img src="6-2320059\823bd3f1-6b17-4404-a933-050d98ff4f4c.jpg" />is function of Rayleigh number. This means the instability vanishes in the non stratified fluid. As a result instability generates plane spiral waves with circular polarization (Beltrami runaway). With increases in amplitude, the instability and its stabilization are described by non linear theory. With <img src="6-2320059\459a0649-b27a-4049-a468-3da2bc72120f.jpg" /> the instability has an essentially non linear character from the very beginning. Stationary equations appear to be hamiltonian that is why they are a rich set of periodical spiral vortex structures. Notwithstanding that attention in this work was essentially paid to the boundary free problem, it should be noted that some periodical solutions turn out to be solutions for the boundary problem with rigid boundaries. One of the most interesting to note are the stationary soliton and kink, which correspond to the separatrix on the phase plane. This is a soliton of the new type. In real space it describes one spiral turn of the velocity vector field around the axe z. The soliton and kink are also the solutions for the boundary problem with free boundaries.</p><p>Let us return to the formulation of the problem. The external helical force <img src="6-2320059\b5d0d4bc-8cd2-4bba-b4b5-f21515ae7944.jpg" /> is given in the explicit form in order to make calculations more transparent. Strictly speaking its explicit form is not very important for the existence of <img src="6-2320059\73d24260-66a9-4c8f-954e-0628f1ce9023.jpg" />-effect itself. It is only necessary that<img src="6-2320059\6881e502-0ad7-4ae4-b8ac-ac22b5f7d4ff.jpg" />. The external force could be chosen statistically with specifying the correlator:</p><disp-formula id="scirp.32662-formula121457"><label>(94)</label><graphic position="anchor" xlink:href="6-2320059\ce55bb38-a8fb-48e1-9d48-24f5ee4e23c0.jpg"  xlink:type="simple"/></disp-formula><p>It is fundamental that the last term <img src="6-2320059\5599312e-0885-4c12-80a4-a606bebf2a97.jpg" /> (helicity) in this correlator is not equal to zero, otherwise the <img src="6-2320059\893195af-8720-4135-b5da-f4b559303703.jpg" />- effect is absent. Nevertheless the statistical method is more bulky since it requires us to specify the functions <img src="6-2320059\61021792-b13b-411b-875f-36aa27f1679d.jpg" /> and calculations of rather complicated integrals. If we specify the external force dynamically then averaging over fast oscillations is performed easily. In conclusion it should be noted that temperature stratification is necessary for the existence of the instability. Previously it was supposed that this stratification was stable. However, the formulae for the large scale instability also admit the transition to an unstable fluid stratification, i.e. allow the substitution <img src="6-2320059\a8ce1017-5654-45ea-8e9c-946f778a342b.jpg" /> But one has to remember that the number <img src="6-2320059\d3ae3ca1-1a08-4e34-815d-f709da1a68cb.jpg" /> has to be sufficiently small so that the usual convective instability should not appear in the system.</p></sec><sec id="s7"><title>REFERENCES</title></sec><sec id="s8"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.32662-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">J. Jimenez, “The Role of Coherent Structures in Modeling Turbulence and Mixing,” Lecture Notes in Physics, Vol. 136, 1981.</mixed-citation></ref><ref id="scirp.32662-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">J. C. McWilliams, “The Emergence of Isolated Coherent Vortices in Turbulent Flow,” Journal of Fluid Mechanics, Vol. 146, 1984, pp. 21-43.  
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