A Numerical Model for Supercritical Flow in Rocket Engine Applications
- Author(s):
- M. Pizzarelli ( University of Rome La Sapienza, Rome, Italy )
- R. Paciorri
- F. Nasuti
- M. Onofri
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
- Ser. no.:
- 2007
- Pub. Year:
- 2007
- No.:
- 2007-5501
- Paper no.:
- AIAA Paper 2007-5501
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200716 [CD-ROM 2007 Disc 16]
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Size Effects on the Performance of Liquid Rocket Engines FED with LH/LOX, LCH4/LOX and KEROSENE/LOX
American Institute of Aeronautics and Astronautics |
3
Conference Proceedings
CFD Analysis of Heat Transfer to Transcritical Fluids in Liquid Rocket Engines
ESA Communication Production Office |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Theoretical analysis and engineering modeling of flowfields in clustered module plug nozzles
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 |