Application of the Implicit MacCormack Scheme for Computation of Supersonic Turbulent Jets Using the Parabolized Navier—Stokes Equations
- Autores: Molchanov A.1, Myakochin A.1, Borovik I.1, Tushkanov A.1
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Afiliações:
- Moscow Aviation Institute
- Edição: Volume 62, Nº 4 (2019)
- Páginas: 633-642
- Seção: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/231167
- DOI: https://doi.org/10.3103/S1068799819040147
- ID: 231167
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Resumo
An effective unconditionally stable numerical method for solving equations describing the flow of supersonic turbulent jets is developed. The method does not require the inversion of block tridiagonal systems of algebraic equations. The results obtained according to this method are in fairly close agreement with the calculations results on the basis of other methods and experimental data.
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Sobre autores
A. Molchanov
Moscow Aviation Institute
Email: myakochinas@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
A. Myakochin
Moscow Aviation Institute
Autor responsável pela correspondência
Email: myakochinas@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
I. Borovik
Moscow Aviation Institute
Email: myakochinas@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993
A. Tushkanov
Moscow Aviation Institute
Email: myakochinas@mai.ru
Rússia, Volokolamskoe sh. 4, Moscow, 125993