Development of a 2D/AXI Kinetic BGK Scheme for Hypersonic Nonequilibrium Flow Compuations
- Author(s):
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2007
- Pub. Year:
- 2007
- No.:
- 2007-0717
- Paper no.:
- AIAA Paper 2007-717
- Pub. info.:
- Reston, Va: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200702 [CD-ROM 2007 Disc 2]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
A Two-Dimensional GasKinetic BGK Scheme for Hypersonic Thermal Non-Equilibirum Flow Computations
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
A One-Dimensional Multiple-Temperature Gas-Kinetic BGK Scheme for Shock Wave Computation
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Efficient Calculations of a Gas-Kinetic BGK Scheme for Inviscid and Viscous Steady Flows
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Hypersonic Aerodynamics using BGK Approach for Oscillatory Membrane-on-Ballute with Bow Shock Wave
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
A kinetic theory based scheme for the numerical solution of the BGK-Burnett equations for hypersonic flows in the continuum-transition regime
American Institute of Aeronautics and Astronautics |