Expansion of the scramjet ground test envelope of the HYPULSE facility
- Author(s):
- Bakos, R.J. ( GASL, Inc. )
- Castrogiovanni, A.
- Calleja, J.F.
- Nucci, L.
- Erdos, J.I.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : International Space Planes and Hypersonic Systems and Technologies Conference
- Ser. no.:
- 1996
- Pub. Year:
- 1996
- No.:
- 96-4506
- Paper no.:
- 96-4506
- Page(from):
- 1
- Page(to):
- 17
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
An experimental and computational study leading to new test capabilities for the HYPULSE facility with a detonation driver
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Design, calibration and analysis of a tunnel mode of operation for the HYPULSE facility
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
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 |
4
Technical Paper
Test facility contaminant and atmospheric ozone effects on hydrocarbon flames and nozzles expansions
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
A technique for mixing measurment in hypervelocity pulse facilities using particle scattering imagery
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |