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        <article-title>Суперкомпьютерные дни в России 2015 // Russian Supercomputing Days 2015 // RussianSCDays.org</article-title>
      </title-group>
      <pub-date>
        <year>2015</year>
      </pub-date>
      <issue>11</issue>
      <fpage>521</fpage>
      <lpage>528</lpage>
      <abstract>
        <p>˝ ¨ 1,</p>
      </abstract>
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      <p>Суперкомпьютерные дни в России 2015 // Russian Supercomputing Days 2015 // RussianSCDays.org
∂f δp
ξα ∂xα = J, J = ν(f + − f ), ν = μ ,
f + = fM 1 + 58 (1 − Pr)Sαcα c2 − 52 , S = nTq3/2 , fM = (πTn)3/2 exp (−c2),
n, nu, 3 nT + nu2, q = Z 1, ξ, ξ2, 1 vv2 f dξ, c = √v , v = ξ − u.</p>
      <p>2 2 T
∂ ∂
∂t f + ∂xα (Ξα ◦ f ) = J , J = ν(f (S) − f ).</p>
      <p>Суперкомпьютерные дни в России 2015 // Russian Supercomputing Days 2015 // RussianSCDays.org</p>
      <p>M (W s−1)(W s − W s−1) = −H(W s−1), s = 1, 2, . . . , M = ∂H .
∂W</p>
      <p>Xi |ein| · |Vi| ≤ 10−5, ein = Xj 1, ξ, ξ2 jT Rinjωα.</p>
      <p>     </p>
      <p>1 0 n
H(W ) = jXN=ξ1  ξξj2j  (fj(S) − fj)ωj +  00  = 0, W =  Tu  .</p>
      <p> vjvj2   2 Pr q   q 
Суперкомпьютерные дни в России 2015 // Russian Supercomputing Days 2015 // RussianSCDays.org
-20
-15
y -10
-5
0
30
20
10
x
0
-10
-20</p>
      <p>Суперкомпьютерные дни в России 2015 // Russian Supercomputing Days 2015 // RussianSCDays.org
Fluids, 36(9):1446 1459, 2007.
5. V.A. Titarev. Conservative numeri al methods for model kineti equations. Computers &amp;
spa e. Physi al Review E, 88:063301, 2013.
7. R.R. Arslanbekov, V.I. Kolobov, A.A. Frolova. Kineti solvers with adaptive mesh in phase
Суперкомпьютерные дни в России 2015 // Russian Supercomputing Days 2015 // RussianSCDays.org
Суперкомпьютерные дни в России 2015 // Russian Supercomputing Days 2015 // RussianSCDays.org
Numerical solution of kinetic equations for high-speed rarefied
gas flows
Vladimir Titarev
Keywords: kinetic equations, unstructured mesh, parallel computing
Analysis of aerodynamics of re-entry vehicles of realistic shape requires the development of
computational methods for rarefied gas flow modeling. The present work is devoted to the
problem of creating efficient parallel method and parallel software to solve the kinetic
equation with the model collision integral of E.M. Shakhov on modern multi-core CPU as
applied to such problems. As a test calculation, the high speed rarefied gas flow over the
reentry space vehicle model of TsAGI is considered.</p>
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