Effect of Airframe Configuration on Airflow Condition to Engine in Hypersonic Flow
- Author(s):
- Publication title:
- A collection of technical papers : 21st AIAA Applied Aerodynamics Conference, Orlando, Florida, 23-26 June 2003
- Title of ser.:
- AIAA Paper : AIAA Applied Aerodynamics Conference
- Ser. no.:
- 2003
- Pub. Year:
- 2003
- Vol.:
- v. 1
- No.:
- 2003-3420
- Paper no.:
- AIAA-2003-3420
- Page(from):
- 188
- Page(to):
- 197
- Pages:
- 10
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISBN:
- 9781563476006 [1563476002]
- Language:
- English
- Call no.:
- A07400/033400 (v.1)
- 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 |
3
Technical Paper
Effect of Ingested Boundary Layer on Scramjet Engine's Thrust and Combustion Characteristics
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 |
11
Technical Paper
Skin-Friction Measurements in Supersonic Combustion Flows of a Scramjet Combustor
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Performance Characteristics of a Scramjet Engine at Mach 10 to 15 Flight Condition
American Institute of Aeronautics and Astronautics |