Aerodynamic Design of Cascade Blades Using Asymptotic Solution of Euler Equations.
- Author(s):
- Publication title:
- AIAA paper
- Title of ser.:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- Ser. no.:
- 2002
- Pub. Year:
- 2002
- No.:
- 2002-0102
- Paper no.:
- 2002-0102
- Pages:
- 12
- Pub. info.:
- American Institute of Aeronautics and Astronautics
- ISSN:
- 01463705
- Language:
- English
- Call no.:
- A07400
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
An Efficient Aerodynamic Design Method Using Asymptotic Solutions of the Euler Equations.
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Design optimization of transonic compressor blades using quasi-3D Navier-Stokes physics
American Institute of Aeronautics and Astronautics |
2
Technical Paper
Aerodynamic Performance Enhancement of Turbomachinery Blades Using 3D Flow Physics
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Inverse Design of 3D Transonic Compressor Blade using 3D Navier-Stokes Flow Physics.
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Analytical Solution of the 2D Euler Equations for Transonic Flow with a Shock Wave
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 |
6
Technical Paper
Shape Optimization of High-Speed Axial Compressor Blades Using 3D Navier-Stokes Flow Physics.
American Society of Mechanical Engineers |
12
Technical Paper
A new approach for efficient construction of asymptotic solutions of the two-dimensional Euler equations
American Institute of Aeronautics and Astronautics |