Investigation of Supersonic Wing Shape Using Busemann Biplane Airfoil
- Author(s):
- M. Yonezawa ( Tohoku University, Sendai, Japan )
- H. Yamashita
- S. Obayashi
- K. Kusunose ( Formerly Tohoku University, Sendai, Japan )
- Publication title:
- AIAA meeting papers on disc
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2007
- Pub. Year:
- 2007
- No.:
- 2007-0686
- Paper no.:
- AIAA Paper 2007-686
- 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 |
7
Technical Paper
Multidisciplinary Design Optimization of Wing Shape for a Small Jet Aircraft Using Kriging Model
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Experimental and Computational Fluid Dynamics Around Supersonic Biplane for Sonic-Boom Reduction
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Numerical Simulation of Supersonic Flow Around Wing- Body Configuration with Integrated Engine Nacelle
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
High-Fidelity Multidisciplinary Design Optimization of Aerostructural Wing Shape for Regional Jet
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Consideration at Off-Design Conditions of Supersonic Flows around Biplane Airfoils
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Transonic Axial-Flow Blade Shape Optimization Using Evolutionary Algorithm and Three-Dimensional Navier-Stoke Solver
American Institute of Aeronautics and Astronautics |