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Simulation study of gust alleviation in a tilt rotor aircraft, volume 1The response to vertical turbulence in cruise of the HTR XV-15 design is studied using simulation techniques. This design is a modified version of the XV-15 with a hingeless fiberglass soft-in-plane rotor system. The parameters of a gust alleviation system are determined and the performance of the system is evaluated over a range of cruise velocities and altitudes.
Document ID
19780005095
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Amos, A. K. (Boeing Vertol Co. Philadelphia, PA, United States)
Alexander, H. R. (Boeing Vertol Co. Philadelphia, PA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1977
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
D210-11231-1
NASA-CR-152050
Report Number: D210-11231-1
Report Number: NASA-CR-152050
Accession Number
78N13038
Funding Number(s)
CONTRACT_GRANT: NAS2-8048
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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