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X-29A forward-swept-wing demonstrator airplaneThe X-29A is a technology demonstrator. The FSW is just one of the technologies. Others include the following: discrete variable camber, relaxed static stability, triplex digital fly-by-wire (FBW) control system, variable-incidence/close-coupled canard, aeroelastically tailored composite wing, and thin supercritical airfoil. The growth potential for additional technologies is shown.
Document ID
19820017333
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Frei, D. R. (Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Publication Information
Publication: NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981
Subject Category
Aerodynamics
Accession Number
82N25209
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19820017320Collected WorksWind-Tunnel/Flight Correlation, 1981
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