Email this article Artificial Dissipation Coefficients in Regularized Equations of Supersonic Aerodynamics
- Authors: Elizarova T.G.1, Shirokov I.A.2
-
Affiliations:
- Keldysh Institute of Applied Mathematics
- Faculty of Computational Mathematics and Cybernetics
- Issue: Vol 98, No 3 (2018)
- Pages: 648-651
- Section: Mathematical Physics
- URL: https://journal-vniispk.ru/1064-5624/article/view/225605
- DOI: https://doi.org/10.1134/S1064562418070141
- ID: 225605
Cite item
Open Access
Access granted
Subscription Access
Abstract
A method for introducing artificial dissipation coefficients into a numerical algorithm based on the quasi-gasdynamic system of equations is proposed. The method applies to aerodynamic flows with large Mach and Reynolds numbers. Simulation results for the supersonic flow over the X-43 aircraft are presented as an illustration. The pressure distribution over the aircraft surface is obtained, which can be used to calculate the aerodynamic characteristics of X-43.
About the authors
T. G. Elizarova
Keldysh Institute of Applied Mathematics
Email: ivanshirokov@inbox.ru
Russian Federation, Moscow, 125047
I. A. Shirokov
Faculty of Computational Mathematics and Cybernetics
Author for correspondence.
Email: ivanshirokov@inbox.ru
Russian Federation, Moscow, 119991
Supplementary files
