The overall problem of achieving dynamic compatibility in helicopter propulsion system can be conveniently divided into four major areas: engine vibration limits; design of the engine/airframe interface; whirling and vibration of power transmission shafting, gearboxes, and bearings; and torsional stability of the engine and drive train with closed-loop fuel controls. These four areas are discussed each with a review of the state of the art and recommendations for future research and development. (Author)
Dynamic Compatibility of Helicopter Propulsion Systems
1972
15 pages
Report
No indication
English
NTIS | 1981
NTIS | 1981
NTIS | 1968
Helicopter Propulsion Systems : Papers
TIBKAT | 1981
Analysis of helicopter propulsion systems
Engineering Index Backfile | 1951
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