Numerical Simulation of High-Temperature Gas Flows in a Millimeter-Scale Thruster
- Author(s):
- Alexeenko,A.A. ( Pennsylvania State University )
- Levin,D.A. ( George Washington University )
- Gimelshein,S.F. ( University of Minnesota )
- Collins,R.J. ( Institute of Theoretical and Applied Mechanics )
- Markelov,G.N.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2001
- Pub. Year:
- 2001
- No.:
- 2001-1011
- Paper no.:
- AIAA-2001-1011
- Page(from):
- 1
- Page(to):
- 10
- Pages:
- 10
- 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 |
2
Technical Paper
Numerical Study of Flow Structure and Thrust Performance for 3-D MEMS-based Nozzles.
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Modeling of Rarefied Hypersonic Flows Over Spacecraft in Martian Atmosphere Using the DSMC Method.
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Statistical Simulation of Laminar Separation in Hypersonic Flows: Numerical Challenges
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Statistical simulation of reactive rarefied flows: numerical approach and applications
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Reconsideration of Flows Through Constriction Microchannels Using the DSMC Method
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Real gas effects on the transition between regular and mach reflections in steady flows
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Statistical simulation of nonequilibrium rarefied flows with quasiclassical VVT transition models
American Institute of Aeronautics and Astronautics |