CFD Simulation of a Rocket-Ejector for an Ejector-Ramjet Combined Cycle Engine
- Author(s):
- Lentsch,A. ( National Aerospace Laboratory of Japan )
- Morgenthaler,V.
- Maita,M.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : International Space Planes and Hypersonic Systems and Technologies Conference
- Ser. no.:
- 2001
- Pub. Year:
- 2001
- No.:
- 2001-1863
- Paper no.:
- AIAA-2001-1863
- Page(from):
- 1
- Page(to):
- 9
- Pages:
- 9
- Pub. info.:
- Reston, VA: 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
Performances of a Rocket Chamber for the Combined-Cycle Engine at Various Conditions
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Performance of a Rocket-Ramjet Combined-Cycle Engine Model in Ejector Mode Operation
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Ram and Ejector-Jet Modes Experiments of the Combined Cycle Engine in Mach 4 Flight Conditions
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Rocket-based combined cycle engine technology development - inlet CFD validation and application
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Rocket-Based Combined Cycle Engine Technology Development: Inlet CFD Validation and Application
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Firing-Tests of a Rocket Combustor for Combined Cycle Engine at Various Conditions
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |