Influence of nozzle geometry on the performance of a pulse detonation engine
- Author(s):
- Stuessy, W.S. ( The University of Texas at Arlington )
- Wilson, D.R.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 1997
- Pub. Year:
- 1997
- No.:
- 97-2745
- Paper no.:
- 97-2745
- Page(from):
- 1
- Page(to):
- 10
- 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 |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Experiments on weakly-ionized air and nitrogen plasmas for hypersonic propulsion facility development
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Experiments on Weakly-Ionized Air and Nitrogen Plasmas for Hypersonic Propulsion Facility Development
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Experimental investigation of an annular multi-cycle pulsed detonation wave engine
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |