This content is not included in your SAE MOBILUS subscription, or you are not logged in.
The General Problems in Vibration of Aircraft Powerplant Components
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1967 by SAE International in United States
Annotation ability available
Some of the more general types of dynamic vibration that exist in aircraft, particularly the powerplant components, are reviewed for reciprocating and turbine engines as well as helicopter and unconventional drive systems. The responsiveness of various components to the source of excitation, resulting in either resonant or nonresonant (forced) vibration, is discussed. The importance of evaluating the fatigue life of a component at varying load conditions, both in the laboratory and field, is stressed.
|MEASUREMENT and PREDICTION of AIRCRAFT VIBRATION
|CRANKSHAFT BENDING VIBRATION
|The Main Rotor Bifilar Absorber and Its Effect on Helicopter Reliability/Maintainability