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A Wind-Tunnel Investigation of Tilt-Rotor Gust Alleviation SystemsThe alleviation of the effects of gusts on tilt rotor aircraft by means of active control systems was investigated. The gust generator, the derivation of the equations of motion of the rotor wing combination, the correlation of these equations with the results of wind tunnel model tests, the use of the equations to design various gust alleviating active control systems, and the testing and evaluation of these control systems by means of wind tunnel model tests were developed.
Document ID
19790017891
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ham, N. D. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Whitaker, H. P. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Aircraft Stability And Control
Report/Patent Number
ASRL-TR-174-7
NASA-CR-152264
Report Number: ASRL-TR-174-7
Report Number: NASA-CR-152264
Accession Number
79N26062
Funding Number(s)
PROJECT: RTOP 505-10-22
CONTRACT_GRANT: NAS2-7262
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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