Application of the Implicit MacCormack Scheme for Computation of Supersonic Turbulent Jets Using the Parabolized Navier—Stokes Equations
- 作者: Molchanov A.1, Myakochin A.1, Borovik I.1, Tushkanov A.1
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隶属关系:
- Moscow Aviation Institute
- 期: 卷 62, 编号 4 (2019)
- 页面: 633-642
- 栏目: 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
如何引用文章
详细
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.
作者简介
A. Molchanov
Moscow Aviation Institute
Email: myakochinas@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
A. Myakochin
Moscow Aviation Institute
编辑信件的主要联系方式.
Email: myakochinas@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
I. Borovik
Moscow Aviation Institute
Email: myakochinas@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
A. Tushkanov
Moscow Aviation Institute
Email: myakochinas@mai.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993