Influence of Downstream Boundary Conditions on Scramjet-Isolator Simulations
- Author(s):
- C. Tam ( AFRL/RZAS/Taitech, Beavercreek, OH )
- D. Eklund ( AFRL/RZAT, WPAFB, OH )
- R. Behdadnia ( AFRL/RZAS, WPAFB, OH )
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA Applied Aerodynamics Conference
- Ser. no.:
- 2008
- Pub. Year:
- 2008
- No.:
- 2008-6929
- Paper no.:
- AIAA 2008-6929
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200810 [CD-ROM 2008 Disc 10]
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Effects of Temperature and Heat Transfer on Shock Train Structures inside Constant-Area Isolators
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Numerical Investigations on Simple Variable Geometry for Improving Scramjet Isolator Performance
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Experimental Investigations on Simple Variable Geometry for Improving Scramjet Isolator Performance
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Characterization of Shock Train Structures inside Constant-Area Isolators of Model Scramjet Combustors
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
CFD Simulations of a 3-D Scramjet Flameholder Using Reduced Chemical Kinetic Mechanisms
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Conditions at the Downstream Boundary for Simulations of Viscous Incompressible Flow
National Aeronautics and Space Adminstration |