Supersonic transitional airfoil shapes of minimum drag
- Author(s):
- Fedorov, A.V. ( Moscow Institute of Physics and Technology )
- Malmuth, N.D. ( Rockwell International Science Center )
- Publication title:
- A collection of technical papers : 15th AIAA Applied Aerodynamics Conference, June 23-25, 1997, Atlanta, GA
- Title of ser.:
- AIAA Paper : AIAA Applied Aerodynamics Conference
- Ser. no.:
- CP978
- Pub. Year:
- 1997
- Vol.:
- pt. 1
- No.:
- 97-2231
- Paper no.:
- AIAA-97-2231
- Page(from):
- 177
- Page(to):
- 193
- Pub. info.:
- Reston, VA: American Institute of Aeronautics and Astronautics
- ISBN:
- 9781563472329 [1563472325]
- Language:
- English
- Call no.:
- (pt.1)A07400/978-1,(pt.2)A07400/978-2
- Type:
- Technical Paper
Similar Items:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Simulation of Supersonic Body Drag Reduction Produced by Forebody Filamentary Plasmas
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Modeling of Forebody Nose Vortex Symmetry Breaking Using Conical Navier-Stokes Solutions
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 |
5
Technical Paper
Parametric Studies of Hypersonic Laminar Flow Control Using a Porous Coating of Regular Microstructure
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Experimental Study of Transition in Hypersonic Boundary Layer on Ultrasonically Absorptive Coating with Random Porosity
American Institute of Aeronautics and Astronautics |
6
Technical Paper
Mechanism of Forebody Nose Vortex Symmetry Breaking Relevant to Plasma Flow Control
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |