Application of the Implicit MacCormack Scheme for Computation of Supersonic Turbulent Jets Using the Parabolized Navier—Stokes Equations
- Авторы: Molchanov A.1, Myakochin A.1, Borovik I.1, Tushkanov A.1
-
Учреждения:
- Moscow Aviation Institute
- Выпуск: Том 62, № 4 (2019)
- Страницы: 633-642
- Раздел: 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
Цитировать
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.
Ключевые слова
Об авторах
A. Molchanov
Moscow Aviation Institute
Email: myakochinas@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
A. Myakochin
Moscow Aviation Institute
Автор, ответственный за переписку.
Email: myakochinas@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
I. Borovik
Moscow Aviation Institute
Email: myakochinas@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
A. Tushkanov
Moscow Aviation Institute
Email: myakochinas@mai.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993