Analysis and Design of Rectangular-Cross-Section Nozzles for Scramjet Engine Testing
- Author(s):
- Gaffney, R. ( NASA Langley Research Center, Hampton, VA )
- Korte, J.
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 42nd
- Pub. Year:
- 2004
- No.:
- 2004-1137
- Paper no.:
- AIAA Paper 2004-1137
- Pub. info.:
- [Reston, Va.]: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200401 [CD-ROM 2004 Disc 1]
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Design of a Mach 3 Nozzle for TBCC Testing in the NASA LaRC 8-Ft High Temperature Tunnel
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Design of a Mach-15 Total-Enthalpy Nozzle With Non-Uniform Inflow Using Rotatioanl MOC
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Design, fabrication, and calibration of a mach 6.5 hypersonic shock tunnel nozzle for scramjet testing applications
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Development and Testing of the Upgraded High Pressure Turbine Section for an Industrial Gas Turbine.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
6
Technical Paper
Parametric Study of Jets Emanating from Serpentine Nozzles of Varied Cross-Section
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Investigation of Low-Reynolds-Number Rocket Nozzle Design Using PNS-Based Optimization Procedure
National Aeronautics and Space Adminstration |