Inducer-Induced Transition in Hypersonic Boundary Layers
- Author(s):
H. Bottini ( von Kármán Institute for Fluid Dynamics, Rhode Saint Genese, Belgium ) F. Jivraj ( von Kármán Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium ) A. Strub S. Paris D. Fletcher C. Asma - Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2007
- Pub. Year:
- 2007
- No.:
- 2007-0537
- Paper no.:
- AIAA Paper 2007-537
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- Language:
- English
- Call no.:
- A07400/200703 [CD-ROM 2007 Disc 3]
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Instantaneous Temperature Imaging in Hypersonic Flows Using Laser-Induced Fluorescence of High Rotational-Quantum-Number Transitions
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
Technical Paper
Experimental Characterization of Hypersonic Boundary Layer in Flight and in Wind-tunnel Condition
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Numerical Investigations of Hypersonic Boundary Layer Transition over Circular Cones
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Space shuttle orbiter aerodynamics induced by asymmetric boundary-layer transition
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
PIV Investigation of Role of Boundary Layer Velocity Fluctuations in Unsteady Shock-Induced Separation
American Institute of Aeronautics and Astronautics |