Shock Jump and Mass Flux Calculations Through Cryogenic Two-phase Flow Nozzle
- Author(s):
- AKMANDOR, I. Sinan ( Department of Aeronautical Engineering Middle East Technical University )
- NAGASHIMA, Toshio
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 1999
- Pub. Year:
- 1999
- No.:
- 99-0347
- Paper no.:
- 99-0347
- 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 |
7
Technical Paper
Multidimensional calculation of two-phase flow in a spray-forming nozzle using eulerian-lagrangian analysis
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
3
Technical Paper
Numerical analysis of rocket turbopump inducer at cryogenic homogeneous two-phase flow conditions
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
4
Technical Paper
Numerical Analysis of Rocket Turbopump Inducer at Cryogenic Homogeneous Two-phase Flow Conditions
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |