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NASA NTRS ยท 19740026401

Engine/airframe interface dynamics experience

Abstract

Problems of engine/drive system torsional stability, engine and output shaft critical speeds, and engine vibration at helicopter rotor order frequencies are discussed, and test data and analyses presented. Also presented is a rotor/drive system dynamics problem not directly related to the engine.

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BibTeXRIS

Fredrickson, C.. 1974-01-01. Engine/airframe interface dynamics experience. https://ntrs.nasa.gov/citations/19740026401

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