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oaioai:casi.ntrs.nasa.gov:19780020113

An analysis of the gust-induced overspeed trends of helicopter rotors

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1978
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Abstract

Equations for analyzing the potential gust-induced overspeed tendency of helicopter rotors are presented. A parametric analysis was also carried out to illustrate the sensitivity of rotor angular acceleration to changes in rotor lift, propulsive force, tip speed, and forward velocity

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This paper was published in NASA Technical Reports Server.

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