Three-dimensional inverse method for turbomachinery blading design
- Author(s):
- Demeulenaere, Alain ( von Karman Institute for Fluid Dymanics )
- Braembussche, Rene Van den
- Publication title:
- A.S.M.E. paper
- Title of ser.:
- ASME Technical Paper : GT
- Ser. no.:
- 1996
- Pub. Year:
- 1996
- No.:
- 96-GT-39
- Paper no.:
- 96-GT-39
- Pub. info.:
- New York: The American Society of Mechanical Engineers
- Language:
- English
- Call no.:
- A11800
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
Application of a three-dimensional inverse method to the design of a centrifugal compressor impeller
The American Society of Mechanical Engineers |
7
Technical Paper
A fully three-dimensional inverse method for turbomachinery balding with Navier-Stokes equations
The American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
8
Technical Paper
A linear approach to the multi-parameter design of three-dimensional turbomachinery blades
American Institute of Aeronautics and Astronautics |
3
Technical Paper
Inverse design of turbomachinery blading for arbitrary blade thickness in three-dimensional transonic flow
The American Society of Mechanical Engineers |
9
Technical Paper
A Linear Approach to the Multi-Parameter Design of Three-Dimensional Turbomachinery Blades
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
5
Technical Paper
Turbomachinery blade design using a Navier-Stokes solver and artificial neural network
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
6
Technical Paper
Inverse design of centrifugal impellers by sumultaneous modification of blade shape and meridional contour
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |