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A survey of active controls benefits to supersonic transportsResults are drawn from studies of the impact of advanced technologies on the design of an arrow-wing configuration. Information presented includes estimated benefits, effects of combinations of active control concepts, and constraints. Emphasis is placed on characteristics that are uniquely related to a large airframe featuring a slender body with a fixed wing of low aspect ratio, high sweep, and small thickness ratio.
Document ID
19760024073
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pratt, K. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Publication Information
Publication: Advanced Control Technol. and its Potential for Future Transport Aircraft
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N31161
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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