A resonance tracking algorithm for the prediction of turbine forced response with friction dampers
- Author(s):
- Breard, C. ( Imperial College of Science, Technology & Medicine )
- Green, J. S.
- Vahdati, M.
- Imregun, M.
- Publication title:
- A.S.M.E. paper
- Title of ser.:
- ASME Technical Paper : GT
- Ser. no.:
- 2000
- Pub. Year:
- 2000
- No.:
- 2000-GT-372
- Paper no.:
- 2000-GT-372
- Pub. info.:
- New York: American Society of Mechanical Engineers
- Language:
- English
- Call no.:
- A11800
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
An integrated time-domain aeroelasticity model for the prediction of fan forced response due to inlet distortion
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
3
Technical Paper
Prediction of high and low engine order forced responses for a low pressure turbine blade
American Institute of Aeronautics and Astronautics |
9
Technical Paper
Wedge Damper Modeling and Forced Response Prediction of Frictionally Constrained Blades.
American Society of Mechanical Engineers |
4
Technical Paper
Forced response analysis of an intermediate pressure turbine blade using a nonlinear aeroelasticity model
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
Technical Paper
Forced Response and Surge Behaviour of IP Core-Compressors with Ice-Damaged Rotor Blades.
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
A Multi-Blade-Row Linearised Analysis Method for Flutter and Forced Response Predictions in Turbomachinery.
American Society of Mechanical Engineers |