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Flight test techniques for the X-29A aircraftThe X-29A advanced technology demonstrator is a single-seat, single-engine aircraft with a forward-swept wing. The aircraft incorporates many advanced technologies being considered for this country's next generation of aircraft. This unusual aircraft configuration, which had never been flown before, required a precise approach to flight envelope expansion. This paper describes the real-time analysis methods and flight test techniques used during the envelope expansion of the X-29A aircraft, including new and innovative techniques that provided for a safe, efficient envelope expansion. The use of integrated test blocks in the expansion program and in the overall flight test approach is discussed.
Document ID
19870035129
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hicks, John W.
(NASA Flight Research Center Edwards, CA, United States)
Cooper, James M., Jr.
(NASA Flight Research Center Edwards, CA, United States)
Sefic, Walter J.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 87-0082
Report Number: AIAA PAPER 87-0082
Accession Number
87A22403
Distribution Limits
Public
Copyright
Other

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