Computational Analysis of Characteristics of Mach Wave Sources in Supersonic Free-Jets
- Author(s):
- T. Nonomura ( University of Tokyo, Sagamihara, Japan )
- K. Fujii ( Japan Aerospace Exploration Agency, Sagamihara, Japan )
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2009
- Pub. Year:
- 2009
- No.:
- 2009-0016
- Paper no.:
- AIAA Paper 2009-0016
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200901
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Computational Analysis of Supersonic Underexpanded Jets Impinging on an Inclined Flat Plate
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Numerical Analysis of the Aerodynamic Characteristics of SSTO Configurations with an Aerospike Nozzle
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Conference Proceedings
Computational Analysis of Characteristics and Mach Number Effects on Noise Emission From Ideally Expanded Highly Supersonic Free-Jet
American Society of Mechanical Engineers |
10
Technical Paper
Computatinal Analysis of the Characteristics of Subsonic, Transonic and Supersonic Base Flows
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Detailed Analysis of Flat Plate Pressure Peaks Created by Supersonic Jet Impingements
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Computational Analysis of Noise Sources Inside Turbulent Boundary Layer Over a Generalized Bump
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |