Comparison of Computational and Experimental Studies on Shock Induced Ignition in Scramjets
- Author(s):
- McGuire, J. ( University of New South Wales, Canberra, Australia )
- Boyce, R.
- Mudford, N.
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : International Space Planes and Hypersonic Systems and Technologies Conference
- Ser. no.:
- 13th
- Pub. Year:
- 2005
- No.:
- 2005-3394
- Paper no.:
- AIAA Paper 2005-3394
- Pub. info.:
- [Reston, Va.]: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200508 [CD-ROM 2005 Disc 8]
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Supersonic combustion - a shock tunnel and vitiation-heated blowdown tunnel comparison
American Institute of Aeronautics and Astronautics |
4
Technical Paper
CFD Analysis of an Ethylene-Fueled Intake-Injection Shock-Induced-Combustion Scramjet Configuration
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Numerical Simulation of Transitional Behaviors in Hypersonic Transverse Jet Interaction
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Scramjet Intake and Exhaust CFD Studies for the HyShot Scramjet Flight Experiment
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |