Real gas effects on the transition between regular and mach reflections in steady flows
- Author(s):
- Gimelshein, S.F. ( Institute of Theoretical and Applied Mechanics, Novosibirsk, Russia )
- Markelov, G.N. ( Institute of Theoretical and Applied Mechanics, Novosibirsk, Russia )
- Ivanov, M.S. ( Institute of Theoretical and Applied Mechanics, Novosibirsk, Russia )
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 1998
- Pub. Year:
- 1998
- No.:
- 98-0877
- Paper no.:
- 98-0877
- Page(from):
- 1
- Page(to):
- 9
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Capsule aerodynamics with real gas effects from free-molecular to near-continum regimes
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Statistical simulation of nonequilibrium rarefied flows with quasiclassical VVT transition models
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Transition Between Regular and Mach Shock Reflections in Plane Overexpanded Jets.
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Statistical simulation of reactive rarefied flows: numerical approach and applications
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Continuum and kinetic simulation of shock wave/laminar boundary layer interaction in hypersonic flows
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Modeling of Rarefied Hypersonic Flows Over Spacecraft in Martian Atmosphere Using the DSMC Method.
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Continuum and Kinetic Simulation of Shock Wave/Laminar Boundary Layer Interaction in Hypersonic Flows
American Institute of Aeronautics and Astronautics |