Design of 3D Transonic Compressor Blades Using Numerical Optimization
- Author(s):
- Chung, J. ( University of Illinois at Urbana-Champaign )
- Shim, J.
- Lee, K. D.
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2000
- Pub. Year:
- 2000
- No.:
- 2000-0227
- Paper no.:
- 00-0227
- Page(from):
- 1
- Page(to):
- 10
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Inverse Design of 3D Transonic Compressor Blade using 3D Navier-Stokes Flow Physics.
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Aerodynamic Performance Enhancement of Turbomachinery Blades Using 3D Flow Physics
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Design Optimization of Transonic Compressor Blades Using Quasi-3D Navier-Stokes Physics
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Aerodynamic Design of Cascade Blades Using Asymptotic Solution of Euler Equations.
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Design optimization of transonic compressor blades using quasi-3D Navier-Stokes physics
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
Shape Optimization of High-Speed Axial Compressor Blades Using 3D Navier-Stokes Flow Physics.
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
12
Technical Paper
Parallelized Design Optimization for Transonic Wings Using Aerodynamic Sensitivity Analysis
American Institute of Aeronautics and Astronautics |