Abstract
Turbomachine blades on spinning and precessing rotors experience gyroscopically induced instabilities and forcing. With vehicle-mounted turbomachines, either constant or harmonic precession occurs, depending on vehicle or mount motion. Responses of uniform cantilever beams at arbitrary stagger, subjected to the noted rotor motion, are predicted in both self-excited and forced-excitation modes taking into account Coriolis acceleration.
Original language | English |
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Pages (from-to) | 342-347 |
Number of pages | 6 |
Journal | Journal of Engineering for Gas Turbines and Power |
Volume | 105 |
Issue number | 2 |
DOIs | |
State | Published - Apr 1983 |