Forced Response of Turbine Engine Bladed Disks and Sensitivity to Harmonic Mistuning.
類似資料:
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
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テクニカルペーパー
Modeling the Effect of Shroud Contact and Friction Dampers on the Mistuned Response of Turbopumps
National Aeronautics and Space Adminstration |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |