Anti‐Vibration Mounting of Aircraft Power Plants: An Analysis of the Problems Associated with Turbojet, Turbo‐Propeller and Reciprocating Engines

Abstract

THE engine and propeller when installed in an airframe transmit various loads to the aircraft structure through the engine mounting. These can be grouped as follows:

Citation

Harriman, J.F. (1959), "Anti‐Vibration Mounting of Aircraft Power Plants: An Analysis of the Problems Associated with Turbojet, Turbo‐Propeller and Reciprocating Engines", Aircraft Engineering and Aerospace Technology, Vol. 31 No. 8, pp. 239-243. https://doi.org/10.1108/eb033147