Application of the Implicit MacCormack Scheme for Computation of Supersonic Turbulent Jets Using the Parabolized Navier—Stokes Equations
- Авторлар: Molchanov A.M.1, Myakochin A.S.1, Borovik I.N.1, Tushkanov A.S.1
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Мекемелер:
- Moscow Aviation Institute
- Шығарылым: Том 62, № 4 (2019)
- Беттер: 633-642
- Бөлім: 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
Дәйексөз келтіру
Аннотация
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.
Негізгі сөздер
Авторлар туралы
A. Molchanov
Moscow Aviation Institute
Email: myakochinas@mai.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
A. Myakochin
Moscow Aviation Institute
Хат алмасуға жауапты Автор.
Email: myakochinas@mai.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
I. Borovik
Moscow Aviation Institute
Email: myakochinas@mai.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
A. Tushkanov
Moscow Aviation Institute
Email: myakochinas@mai.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
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