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Research opportunities for rotorcraftThe control of structural vibration is helicopters is discussed. Active control concepts, wind tunnel tests, rotor vibratory loads, systems integration, and engine control are among the topics discussed.
Document ID
19840012528
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Blake, B. B. (Boeing Vertol Co. Philadelphia, PA, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1984
Publication Information
Publication: NASA. Langley Research Center NASA Aircraft Controls Research, 1983
Subject Category
Aircraft Design, Testing And Performance
Accession Number
84N20596
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19840012499Collected WorksNASA Aircraft Controls Research, 1983
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