Numerical simulation of the pseudo-shock region formation in the channel-Reference-Cited by-同舟云学术

Numerical simulation of the pseudo-shock region formation in the channel

Published:2016 Issue:2 Volume: Page:1-24
ISSN:2071-2898
Container-title:Keldysh Institute Preprints
language:
Short-container-title:KIAM Prepr.

Author:

Borisov Vitaly Evgenyevich¹^ORCID,Kudryashov Ivan Yurievich¹^ORCID,Lutsky Alexander Evgenievich¹

Affiliation:

1. Keldysh Institute of Applied Mathematics

Publisher

Keldysh Institute of Applied Mathematics

Subject

General Medicine

Reference22 articles.

1. О.В. Гуськов, В.И. Копченов, И.И. Липатов, В.Н. Острась, В.П. Старухин. Процессы торможения сверхзвуковых течений в каналах. М.: ФИЗМАЛИТ, 2008.

2. J. Anderson. Hypersonic and high-temperature gas dynamics, Second edition, AIAA, 2006.

3. D. Andreadis. Scramjet Engines Enabling the Seamless Integration of Air & Space Operations // The Industrial Physicist, August/September 2004.

4. В.А. Забайкин. Управление псевдоскачком нестационарным воздействием // Физико-химическая кинетика в газовой динамике, 2011, Т.12. 7 c. http://chemphys.edu.ru/issues/2011-12/articles/353/

5. R.C. Mutzman, J.S. Murphy. X-51 Development: A Chief Engineer’s Perspective // 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 13 April 2011.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Calculation of High-Speed Flows Based on a Hyperbolic Quasi-Gas-Dynamic System;Mathematical Models and Computer Simulations;2022-09-22

2. Experimental-theoretical study of pressure distribution along the wall when a supersonic gas flow moves in an axisymmetric channel with sudden expansion;Thermophysics and Aeromechanics;2022-01

3. Simulation of transition between regular and Mach shock waves reflections by an implicit scheme based on the LU-SGS and BiCGStab methods;Keldysh Institute Preprints;2016

4. Active impact on the flow around hypersonic flying vehicles;Keldysh Institute Preprints;2016