Scramjet testing in the T4 impulse facility
- Author(s):
- Paull, A. ( Centre for Hypersonics, Department of Mechanical Engineering, The University of Queenland )
- Stalker, R.J. ( Centre for Hypersonics, Department of Mechanical Engineering, The University of Queenland )
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : International Space Planes and Hypersonic Systems and Technologies Conference
- Ser. no.:
- 1998
- Pub. Year:
- 1998
- No.:
- 98-1533
- Paper no.:
- 98-1533
- 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 |
2
Technical Paper
A shock tunnel investigation of scramjet performance with partially premixed combustion
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
10
Technical Paper
Design, fabrication, and calibration of a mach 6.5 hypersonic shock tunnel nozzle for scramjet testing applications
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Scramjet Intake and Exhaust CFD Studies for the HyShot Scramjet Flight Experiment
American Institute of Aeronautics and Astronautics |