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Historical review of C-5A lift distribution control systemsAnalytical and experimental development work on various load alleviation systems for the C-5A is reviewed to trace the development of the technical and hardware concepts to the present time. Variations in system objectives, means of implementation and effects on loads and airplane performance, stability and control are discussed.
Document ID
19760024059
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Disney, T. E. (Lockheed Aircraft Corp. Marietta, GA, United States)
Eckholdt, D. C. (Wright-Patterson AFB Ohio, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Publication Information
Publication: NASA. Dryden Flight Res. Center Advanced Control Technol. and its Potential for Future Transport Aircraft
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N31147
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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