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	<title>Электронный научно-практический журнал «Современная техника и технологии» &#187; air dynamics.</title>
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		<title>Solution of problems of air protection in the Comsol Multiphysics (for example, diffusion of biogas from landfills). Using Comsol Script ™</title>
		<link>https://technology.snauka.ru/en/2013/10/2412</link>
		<comments>https://technology.snauka.ru/en/2013/10/2412#comments</comments>
		<pubDate>Mon, 14 Oct 2013 13:04:30 +0000</pubDate>
		<dc:creator>artursauc</dc:creator>
				<category><![CDATA[Common rubric]]></category>
		<category><![CDATA[air dynamics.]]></category>
		<category><![CDATA[air pollution]]></category>
		<category><![CDATA[biogas]]></category>
		<category><![CDATA[Comsol Multiphysics]]></category>
		<category><![CDATA[Comsol Script]]></category>
		<category><![CDATA[Convection and diffusion]]></category>
		<category><![CDATA[finite element/volume analysis]]></category>

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		<description><![CDATA[ The software package Comsol Multiphysics, which implements the numerical solution of equations of mathematical physics, partial (PDE) by finite element/volume, is now widely used to solve problems in various fields of science and technology. The advantages of this package is that it supports a programming language Comsol Script, which allows you to specify non-trivial initial [...]]]></description>
			<content:encoded><![CDATA[<p><span> The software package Comsol Multiphysics, which implements the numerical solution of equations of mathematical physics, partial (PDE) by finite element/volume, is now widely used to solve problems in various fields of science and technology. The advantages of this package is that it supports a programming language Comsol Script, which allows you to specify non-trivial initial and boundary conditions , the physical parameters of the environment , to work together various modules package Comsol Multiphysics [1] . In this paper, the language of the Comsol Script written a program using which in Comsol Multiphysics solved urgent task of Applied Ecology &#8211; Mathematical modeling of air pollution biogas , outstanding in the decomposition of solid waste and industrial waste in landfills.<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;">Dissipation in the atmospheric surface layer with a passive tracer concentration, mg per m<sup>3</sup>, described by unsteady turbulent diffusion equation:<br />
</span></p>
<p style="text-align: right;"><img style="margin-top: -10px; margin-bottom: -10px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu1.png" alt="" width="216" height="48" /><span style="color: black;">                                                                                          (1)<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;">there <img style="margin-top: -15px; margin-bottom: -15px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu2.png" alt="" width="77" height="36" /> is vector velocity, m per sec; <em>w<sub>s</sub></em> is sedimentation rate impurities: for light inert gas impurities <em>w<sub>s</sub></em>=0 m per sec; for heavy <em>w<sub>s </sub></em>= 0,001 m per sec; for aerosols <em>w<sub>s</sub></em> = 0,008 m per sec [2]; <em>k<sub>хуz</sub></em> is coefficient of turbulent viscosity in different directions, m<sup>2</sup> per sec; <img style="margin-top: -19px; margin-bottom: -19px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu3.png" alt="" width="38" height="32" /> is function emissions of impurities in the atmosphere, which is determined by the equation:<br />
</span></p>
<p style="text-align: right;"><img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu4.png" alt="" width="148" height="47" /><span style="color: black;">                                                                                                (2)<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;">There <em>I<sub>i</sub></em> is function emissions from <em>i</em>-th source; <em>f<sub>i </sub></em>(<em>t</em>) and <img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu5.png" alt="" width="39" height="39" /> are functions describing the mode of operation and location of stationary sources, connected to the radius-vector <img style="margin-top: -19px; margin-bottom: -19px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu6.png" alt="" width="10" height="34" /> and <img style="margin-top: -19px; margin-bottom: -19px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu7.png" alt="" width="74" height="34" />. For continuously operating sources <em>f<sub>i </sub></em>(<em>t</em>) = 1.<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;">Because the movement of air is a subsonic, in accordance with the approximation of the Boussinesq approximation can be described by a system of equations of the Navier-Stokes equations for an incompressible viscous fluid:</span></p>
<p style="text-align: justify;"><span style="color: black;"><br />
</span></p>
<p style="text-align: right;"><img style="margin-top: -40px; margin-bottom: -40px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu8.png" alt="" width="277" height="83" /><span style="color: black;">                                                                            (3)<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;"><span>There </span><span>n is dynamic viscosity, Pa·sec; </span><span><em>р</em></span><span> is piezometric pressure, Pa;  p </span><span>is the density of the medium (air), kg per m<sup>3</sup>; <img style="margin-top: -18px; margin-bottom: -18px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu9.png" alt="" width="13" height="31" /> is specific force field, N/m<sup>3</sup>.<br />
</span></span></p>
<p style="text-align: justify;"><span style="color: black;">Density of air can be found using the equation of state of an ideal gas:<br />
</span></p>
<p style="text-align: right;"><img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu10.png" alt="" width="112" height="41" /><span style="color: black;">                                                                                                            (4)<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;"><span>There </span><span><em>р</em><sub>атм</sub></span><span> is atmospheric pressure, Pа; </span><span><em>R</em><span><sub>m</sub></span></span><span> is gas constant, for air </span><span><em>R</em><sub><span>m </span></sub></span><span>= 3,464<span>×</span>10<sup>-3 </sup>J per kg<span>×</span>K<span>×</span>mol;</span><span><em> Т</em><sub>ф </sub></span><span>is background temperature, K.<br />
</span></span></p>
<p style="text-align: justify;"><span style="color: black;">Kinematic viscosity can be found using the approximation [3]:<br />
</span></p>
<p style="text-align: right;"><span style="color: black;"><span><span>h</span> = 6<span>×</span>10<sup>-6 </sup>+ 4<span>×</span>10<sup>-8</sup><span>×</span><em>Т</em><sub>ф</sub>.                                                                                                     </span><span>(5)<br />
</span></span></p>
<p style="text-align: justify;"><span style="color: black;">Turbulent flow structure, which cannot be solved explicitly for the numerical solution of a system of Navier-Stokes equations, are approximated using the subgrid turbulence Smagorinsky model. This approach proposed by Deardorff and developed in the works of Smagorinsky, involves the allocation of the scale, smaller grid, which is approximated by the turbulence [4]. The preference of this model is given to the fact that it takes into account the presence of turbulence, formed a small vortices while flowing wind flow walls of buildings, structures and other obstacles, but the vortices don&#8217;t need to approximate the «wall-functions». This approach due to the reduction of the dimension of the matrix equations by a sequence of calculations reduces the requirements to computing resources of a computer.<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;"><span>The scale of small eddies in the Smagorinsky model determined time-measures </span><span><span>D</span><em>х</em></span><span>, </span><span><span>D</span><em>у</em></span><span>, </span><span><span>D</span><em>z</em></span><span> three-dimensional cell:<br />
</span></span></p>
<p style="text-align: right;"><img style="margin-top: -21px; margin-bottom: -21px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu11.png" alt="" width="104" height="37" /><span style="color: black;">                                                                                                           (6)<br />
</span></p>
<p><span style="color: black;">The coefficients of turbulent viscosity is determined using the system:</span><span style="color: black;"><br />
</span></p>
<p style="text-align: right;"><img style="margin-top: -10px; margin-bottom: -10px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu12.png" alt="" width="133" height="99" /><span style="color: black;">                                                                                                            (7)</span></p>
<p style="text-align: justify;"><span style="color: black;"><span>There </span><span><em>k</em><sub>баз</sub></span><span> is basic coefficient of turbulent viscosity, and contempt of the temperature gradient low altitude and temperature of the discharged impurities determined the approximate equation:</span></span></p>
<p style="text-align: justify;"><span style="color: black;"><span><br />
</span></span></p>
<p style="text-align: right;"><img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu13.png" alt="" width="131" height="62" /><span style="color: black;">                                                                                                  (8)<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;"><span>There </span><span><em>k</em><sub>ф </sub></span><span>is background coefficient of turbulent viscosity, </span><span><em>k</em><sub>ф</sub></span><span> = 1-15 м<sup>2</sup>/с; </span><span>ε</span><span> = 0,1-0,4; </span><span><em>Def </em>(<em>x</em>; <em>y</em>; <em>z</em>)</span><span> is function of deformation or dissipation defined by the equation:<br />
</span></span></p>
<p style="text-align: center;"><img class="aligncenter" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu14.png" alt="" width="477" height="72" /><br />
<span style="color: black;">At the upstream boundary of the computational domain profile of wind speed is given by Karman. Since wind flow can be directed at an angle of the input boundary of the computational domain, the velocity components of the system are given by:</span></p>
<p style="text-align: center;"><span style="color: black;"><br />
</span></p>
<p style="text-align: right;"><img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu15.png" alt="" width="234" height="89" /><span style="color: black;">                                                                    (9)<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;"><span>There </span><span><em>u*</em></span><span> is dynamic speed, m per sec; <em>z</em><sub>0</sub> is argument of a roughness; <img style="margin-top: -15px; margin-bottom: -15px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu16.png" alt="" width="9" height="28" /> is Karman`s constant,<img style="margin-top: -19px; margin-bottom: -19px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu17.png" alt="" width="41" height="31" />; <em>Н</em><sub>ср</sub> is the average height of wind barriers; </span><span><em>С</em></span><span> is coefficient of resistance;</span></span><span><br />
</span><span>α</span><span> is the angle between the direction of the wind on the input in the computational domain boundary and the x-axis, radian.<span style="color: black;"><br />
</span></span></p>
<p style="text-align: justify;"><span style="color: black;">At the downstream boundary of the computational domain is given the type of border Outlet, the boundary condition Normal flow / zero pressure:<br />
</span></p>
<p style="text-align: right;"><span style="color: black;"><span><em>р</em> = 0.                                                                                                         </span><span> (10)<br />
</span></span></p>
<p style="text-align: justify;"><span style="color: black;">On the surfaces of buildings and structures, landfill, land for the components of the wind speed is given by the condition of impermeability and adhesion:<br />
</span></p>
<p style="text-align: right;"><img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu18.png" alt="" width="33" height="32" /><span style="color: black;"><span>                                                                                                            (11)<br />
</span></span></p>
<p style="text-align: justify;"><span style="color: black;"><span>If the streamlined surface is the area where is blowing (suction) air velocity components </span><span><em>u</em><sub>в</sub></span><span>, </span><span><em>v</em><sub>в</sub></span><span>, </span><span><em>w</em><sub>в</sub></span></span><span style="color: black;">, then the area is given by the boundary condition Moving /Leaking wall:<br />
</span></p>
<p style="text-align: right;"><span style="color: black;"><span><em>и</em> = <em>и</em><sub>в</sub>; <em>v = v</em><sub>в</sub>;<em> w = w</em><sub>в</sub>.</span><span>                                                                                          (12)<br />
</span></span></p>
<p style="text-align: justify;"><span style="color: black;">On the lateral boundaries of the computational domain is specified Symmetry boundary, meaning the absence of leaks and tangential stresses:<br />
</span></p>
<p style="text-align: right;"><img style="margin-top: -15px; margin-bottom: -15px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu19.png" alt="" width="216" height="34" /><span style="color: black;">                                                                               (13)<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;">There <img style="margin-top: -15px; margin-bottom: -15px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu20.png" alt="" width="11" height="29" /> and <img style="margin-top: -15px; margin-bottom: -15px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu21.png" alt="" width="10" height="29" /> is normal and tangential unit vector to the boundary surface, unit vector <img style="margin-top: -15px; margin-bottom: -15px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu22.png" alt="" width="11" height="29" /> directed outward from the boundary region.<br />
</span></p>
<p style="text-align: justify;"><span>At presence on a surface of the polygon of ground insulation filling and absence of gas drainage wells circuit equations emissions and diffusion components of biogas is produced with the help of the derived equations [5]:</span></p>
<p style="text-align: justify;"><span><span style="color: black;"><br />
</span></span></p>
<p style="text-align: right;"><img style="margin-top: -15px; margin-bottom: -15px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu23.png" alt="" width="193" height="55" /><span style="color: black;">                                                                                     (14)<br />
</span></p>
<p style="text-align: justify;"><span>There<em> D</em> is diffusivity of landfilling (insulating the outside waste), m<sup>2</sup> per sec; <em>h</em> is thickness of landfilling, m; <em>n</em><sub>отх</sub> is porosity of waste, <em>n</em><sub>отх </sub>= 0,33; γ is permeation coefficient, for gases γ = 0,01-0,015 m per sec; <em>с</em><sub>пов,возд</sub> is the concentration of component biogas at the upper side of air filling, mg per <span style="color: black;">m<sup>3</sup></span>.<span style="color: black;"><br />
</span></span></p>
<p style="text-align: justify;"><span style="color: black;">On the surface of the landfill to calculate the concentration of a component of biogas in the absence of gas drainage wells gets <img style="margin-top: -18px; margin-bottom: -18px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu24.png" alt="" width="59" height="31" /> and sets boundary condition:<br />
</span></p>
<p style="text-align: right;"><span style="color: black;"><span><em>c </em>= <em>с</em><sub>пов,возд</sub></span><sub><span>.</span></sub><span>                                                                                                 (15)<br />
</span></span></p>
<p style="text-align: justify;"><span style="color: black;">If the emission biogas through gas drainage wells or surface landfill, which has no insulating filling, the consideration of the effect of each of them by using boundary condition Flux:<br />
</span></p>
<p style="text-align: right;"><img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu25.png" alt="" width="124" height="39" /><span style="color: black;">                                                                                        (16)<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;"><span>On impervious surfaces flow of impurities (</span><span><em>I<sub>i</sub></em> = 0</span><span>) is given by boundary condition Isolation/Symmetry:<br />
</span></span></p>
<p style="text-align: right;"><img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu26.png" alt="" width="121" height="41" /><span style="color: black;">                                                                                         (17)<br />
</span></p>
<p style="text-align: justify;"><span style="color: black;">On the other boundaries of the computational domain is given by the boundary condition Convective flux:<br />
</span></p>
<p style="text-align: right;"><img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu27.png" alt="" width="99" height="37" /><span style="color: black;">                                                                                              (18)<br />
</span></p>
<p>When determining the scale of small eddies in the model of the radical work of Smagorinsky D<em>х</em>D<em>у</em>D<em>z</em> can be interpreted as the volume of the rectangular cell using MCS . When using the finite element method with the most common type of cells &#8211; tetrahedral most famous software packages such as Ansys CFX, Fluent, Flow Vision, etc. In this case, the volume of each cell is calculated by means of numerical methods. To determine the scale, the following simpler approach. The maximum linear dimension of the finite element and should be much smaller than the calculated area, the growth rate of the element responsible for the degree of condensation, taken strictly to 1. These options allow you to get a thick, almost uniform grid consisting of a set of tetrahedral that are close to correct. Then, in our case for small scale vortices can be approximated as the cube root of the volume of the tetrahedron:</p>
<p><img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101813_1645_1.png" alt="" width="209" height="39" />                                                                     (19)<br />
Then, using the approximation<img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101813_1645_2.png" alt="" width="99" height="33" />, we obtain:<em><br />
</em></p>
<p><img style="margin-top: -20px; margin-bottom: -20px;" src="https://technology.snauka.ru/wp-content/uploads/2013/10/101813_1645_3.png" alt="" width="226" height="40" />                                                                 (20)</p>
<p>In our case, made ​​<em>a</em> = 4 m. At this density grid in [6] by the method of successive approximations for calculating the concentrations of methane emitted at the site &#8221; Centralny&#8221; in Volgograd , the optimal values ​​of <em>k</em><sub>ф</sub> = 4 m<sup>2</sup>/s ; ε = 0,2. This approach eliminates the calculation of sub-grid scale using tetrahedral finite element mesh, thereby simplifying the numerical (software) implementation of the turbulence model and reduces the requirements for compute-intensive computer.</p>
<p>From a practical point of view is suitable stationary statement of the problem. In this case, a method of determining where the problem is solved on a large time interval that the process leads to stationary. Implicit scheme allows to get rid of restrictions to the size of the time step. Stationary statement of the problem significantly reduces the number of iterations, and the consumption of computing resources of a computer.</p>
<p>The solution of the discrete analogues of the differential equations made by bi-conjugate gradients with the stabilization of the solution. The whole program code is more than a dozen pages, so in an article for the sake of brevity, it shows only the main conclusions:</p>
<p style="text-align: justify;"><span><span style="color: forestgreen;">% COMSOL Multiphysics Model M-file</span><br />
</span></p>
<p><span><span style="color: forestgreen;">% Generated by COMSOL 3.4 (COMSOL 3.4.0, $Date: 2007/10/03 17:02:19 $)</span><br />
</span></p>
<p><span style="color: black;"><span>flclear <span style="color: #a020f0;">fem</span></span><br />
</span></p>
<p><span><span style="color: forestgreen;">% COMSOL version</span><br />
</span></p>
<p><span style="color: black;"><span>clear <span style="color: #a020f0;">vrsn</span></span><br />
</span></p>
<p><span style="color: black;"><span>vrsn.name = <span style="color: #a020f0;">&#8216;COMSOL 3.4&#8242;<span style="color: black;">;</span></span></span><br />
</span></p>
<p><span style="color: black;"><span>vrsn.ext = <span style="color: #a020f0;">&#8216;a&#8217;<span style="color: black;">;</span></span></span><br />
</span></p>
<p><span><span style="color: black;">vrsn.major = 0;</span><br />
</span></p>
<p><span><span style="color: black;">vrsn.build = 603;</span><br />
</span></p>
<p><span style="color: black;"><span>vrsn.rcs = <span style="color: #a020f0;">&#8216;$Name: $&#8217;<span style="color: black;">;</span></span></span><br />
</span></p>
<p><span style="color: black;"><span>vrsn.date = <span style="color: #a020f0;">&#8216;$Date: 2007/10/03 17:02:19 $&#8217;<span style="color: black;">;</span></span></span><br />
</span></p>
<p><span><span style="color: black;">fem.version = vrsn;</span><br />
</span></p>
<p><span><span style="color: forestgreen;">% Constants</span><br />
</span></p>
<p><span style="color: black;"><span>% Constants<br />
fem.const = {&#8216;W_s&#8217;,&#8217;0&#8242;, &#8230;<br />
&#8216;k_f&#8217;,&#8217;4&#8242;, &#8230;<br />
&#8216;epsilon&#8217;,&#8217;0.2&#8242;, &#8230;<br />
&#8216;Mcomp&#8217;,&#8217;5&#8242;, &#8230;<br />
&#8216;h_iz&#8217;,&#8217;0.2&#8242;, &#8230;<br />
&#8216;Vpol&#8217;,&#8217;100000&#8242;, &#8230;<br />
&#8216;Diffusiv&#8217;,&#8217;3.4e-5&#8242;, &#8230;<br />
&#8216;gamma&#8217;,&#8217;0.001&#8242;, &#8230;<br />
&#8216;Ccomp&#8217;,&#8217;50&#8242;, &#8230;<br />
&#8216;Pamb&#8217;,&#8217;1e5&#8242;, &#8230;<br />
&#8216;T_amb&#8217;,&#8217;25&#8242;, &#8230;<br />
&#8216;Udin&#8217;,&#8217;3&#8242;, &#8230;<br />
&#8216;Hsr&#8217;,&#8217;10&#8242;, &#8230;<br />
&#8216;Z0&#8242;,&#8217;0.2&#8242;, &#8230;<br />
&#8216;C&#8217;,&#8217;0.0115&#8242;, &#8230;<br />
&#8216;alpha&#8217;,&#8217;0&#8242;, &#8230;<br />
&#8216;a&#8217;,&#8217;4&#8242;};</span></span></p>
<p>% Geometry</p>
<p>% (Default values are not included)</p>
<p>% Application mode 1<br />
clear appl<br />
appl.mode.class = &#8216;FlNavierStokes&#8217;;<br />
appl.shape = {&#8216;shlag(1,&#8221;u&#8221;)&#8217;,'shlag(1,&#8221;v&#8221;)&#8217;,'shlag(1,&#8221;w&#8221;)&#8217;,'shlag(1,&#8221;p&#8221;)&#8217;};<br />
appl.gporder = 2;<br />
appl.cporder = 1;<br />
appl.assignsuffix = &#8216;_ns&#8217;;<br />
clear prop<br />
prop.analysis=&#8217;static&#8217;;<br />
appl.prop = prop;<br />
clear pnt<br />
pnt.p0 = {};<br />
pnt.name = {};<br />
pnt.pnton = {};<br />
pnt.ind = [];<br />
appl.pnt = pnt;<br />
clear bnd<br />
bnd.U0out = {};<br />
bnd.v0 = {};<br />
bnd.opentype = {};<br />
bnd.u0 = {};<br />
bnd.Fbnd = {};<br />
bnd.p0 = {};<br />
bnd.type = {};<br />
bnd.velType = {};<br />
bnd.walltype = {};<br />
bnd.w0 = {};<br />
bnd.inttype = {};<br />
bnd.vw = {};<br />
bnd.U0in = {};<br />
bnd.ww = {};<br />
bnd.uw = {};<br />
bnd.name = {};<br />
bnd.outtype = {};<br />
bnd.f0 = {};<br />
bnd.intype = {};<br />
bnd.stresstype = {};<br />
bnd.ind = [];<br />
appl.bnd = bnd;<br />
clear equ<br />
equ.eta = &#8217;6e-6+T_amb*4e-8&#8242;;<br />
equ.name = &#8216;physical parameters of the atmosphere in the zone of landfill&#8217;;<br />
equ.rho = &#8216;Pamb*3.464e-3/T_amb&#8217;;<br />
equ.ind = [];<br />
appl.equ = equ;<br />
fem.appl{1} = appl;</p>
<p>% Application mode 2<br />
clear appl<br />
appl.mode.class = &#8216;FlConvDiff&#8217;;<br />
appl.assignsuffix = &#8216;_cd&#8217;;<br />
clear prop<br />
prop.analysis=&#8217;static&#8217;;<br />
clear weakconstr<br />
weakconstr.value = &#8216;off&#8217;;<br />
weakconstr.dim = {&#8216;lm5&#8242;};<br />
prop.weakconstr = weakconstr;<br />
appl.prop = prop;<br />
clear bnd<br />
bnd.d = {};<br />
bnd.Dbnd = {};<br />
bnd.c0 = {};<br />
bnd.name = {};<br />
bnd.N = {};<br />
bnd.type = {};<br />
bnd.ind = [];<br />
appl.bnd = bnd;<br />
clear equ<br />
equ.D = &#8217;4.160167646*k_f+0.707106781*epsilon*(a^2)*((ux)^2+(vy)^2+(wz)^2+0.5*((vx+uy)^2+(wy+vz)^2+(uz+wx)^2))^0.5&#8242;;<br />
equ.w = &#8216;w-W_s&#8217;;<br />
equ.v = &#8216;v&#8217;;<br />
equ.u = &#8216;u&#8217;;<br />
equ.name = &#8216;physical parameters of the atmosphere in the zone of landfill&#8217;;<br />
equ.ind = [];<br />
appl.equ = equ;<br />
fem.appl{2} = appl;<br />
fem.sdim = {&#8216;x&#8217;,'y&#8217;,'z&#8217;};<br />
fem.frame = {&#8216;ref&#8217;};<br />
fem.border = 1;<br />
clear units;<br />
units.basesystem = &#8216;SI&#8217;;<br />
fem.units = units;</p>
<p>% Scalar expressions<br />
fem.expr = {&#8216;profil_u&#8217;,&#8217;2.5*Udin*log((z-Hsr+Z0/C)/Z0)*cos(alpha)&#8217;, &#8230;<br />
&#8216;profil_v&#8217;,&#8217;2.5*Udin*log((z-Hsr+Z0/C)/Z0)*sin(alpha)&#8217;, &#8230;<br />
&#8216;Cpov&#8217;,'(Mcomp*z_iz*h_izol/Vpol+0.33*Diffusiv*Ccomp)/(Diffusiv+gamma*h_iz)&#8217;, &#8230;<br />
&#8216;Mud&#8217;,'Mcomp*z/Vpol&#8217;};</p>
<p>% Descriptions<br />
clear descr<br />
descr.expr= {&#8216;Mud&#8217;,'emission component of biogas from the landfill area, mg / (kv.m.sek) (boundary condition of the 2nd kind is used in the absence of landfilling)&#8217;,'Cpov&#8217;,'concentration of the component of biogas at the landfill surface (boundary condition of the 2nd kind is used in the absence of landfilling)&#8217;,'profil_v&#8217;,'y-oic wind component on the input boundary of the computational domain&#8217;,'profil_u&#8217;,'x-oic wind component on the input boundary of the computational domain&#8217;};<br />
fem.descr = descr;</p>
<p>% Descriptions<br />
descr = fem.descr;<br />
descr.const= {&#8216;h_iz&#8217;,'thickness of the insulating filling (default made ??0.2 m)&#8217;,'Pamb&#8217;,'atmospheric pressure Pa&#8217;,'Vpol&#8217;,'volume occupied by the solid waste landfill or softwareб cubic m&#8217;,'Hsr&#8217;,'average height of wind barriers, m&#8217;,'Diffusiv&#8217;,'diffusivity of the soil from which the filling,square m/seс&#8217;,'a&#8217;,'maximum line size tetraedricheskogo finite element, m&#8217;,'C&#8217;,'roughness parameter&#8217;,'k_f&#8217;,'background coefficient eddy viscosity Smagorinsky model, square m/sec (default is assumed to be 4)&#8217;,'Mcomp&#8217;,'emission component of the biogas emitted from around the landfill or software mg/sec&#8217;,'Udin&#8217;,'dynamic speed, m/s&#8217;,'Z0&#8242;,&#8217;resistance coefficient, m&#8217;,'W_s&#8217;,'settling velocity of the impurities in the atmosphere for light inert gas impurities 0; Heavy 0.001, 0.008 for aerosols m/sec&#8217;,'Ccomp&#8217;,'the concentration of the components in the biogas at the time of its release in the body of the landfill, mg/cubic m&#8217;,'gamma&#8217;,'coefficient of gas seepage through the soil, m/sec (default is 0.001)&#8217;,'alpha&#8217;,'angle between the direction of the wind at the entrance to the settlement area boundary and the x axis, radian&#8217;,'epsilon&#8217;,'constant in the Smagorinsky model (the default is assumed to be 0.2)&#8217;,'T_amb&#8217;,'background air temperature, K&#8217;};<br />
fem.descr = descr;</p>
<p>% ODE Settings<br />
clear ode<br />
clear units;<br />
units.basesystem = &#8216;SI&#8217;;<br />
ode.units = units;<br />
fem.ode=ode;</p>
<p>% Multiphysics<br />
fem=multiphysics(fem);<span><br />
</span></p>
<p style="text-align: justify;"><span style="color: black;">The settlements were made on the computer AMD FX™-4100 Quard-Core Processor, RAM 4 Gb, 3,2 GHz, OS MS Windows 7 Ultimate SP1. The calculation time for landfill «Centralny» was about 30 hours. The results of calculations are shown in figures 1-2 (unit mol per m<sup>3</sup> treated as mg per m<sup>3</sup>).<br />
</span></p>
<p style="text-align: center;"><img src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu30.jpg" alt="" /><span style="color: black;"><br />
</span></p>
<p style="text-align: center;"><span>Figure<span style="color: black;"> 1 – The field of wind speed, m per sec, at the height of 1.8 m above the top of the landfill site landfill PTO-3 «Novosyolki» 26.08.2001<br />
</span></span></p>
<p style="text-align: center;"><img src="https://technology.snauka.ru/wp-content/uploads/2013/10/101413_1304_SautsAVSolu31.jpg" alt="" /><span style="color: black;"><br />
</span></p>
<p style="text-align: center;"><span>Figure 2<span style="color: black;"> – Field concentrations of methane, mg per m<sup>3</sup>, at the height of 1.8 m above the top of the landfill site PTO-3 «Novosyolki» 26.08.2001</span></span></p>
<p><span><br />
</span></p>
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