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X-29 Flight Test Program including wind tunnel and computational supportA cooperative effort has been defined between NASA-Ames/Dryden Flight Research Facility and NASA-Langley Research Center in support of the X-29A Advanced Technology Demonstrator. The effort involves three phases: flight testing, wind-tunnel testing in the National Transonic Facility, and computational support of each experimental phase. These efforts are primarily aimed at understanding the complex flow phenomena and component interactions associated with the X-29A. Each phase of the effort is discussed in detail and initial data comparisons are presented. In summary, the synergistics effects of the complementary phases are identified, which will enhance the understanding of the unique aerodynamics of the X-29A.
Document ID
19870045310
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Waggoner, E. G.
(NASA Langley Research Center Hampton, VA, United States)
Jennett, L. A.
(NASA Flight Research Center Edwards, CA, United States)
Bates, B. L.
(Vigyan Research Associates, Inc. Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
SAE PAPER 861642
Report Number: SAE PAPER 861642
Accession Number
87A32584
Distribution Limits
Public
Copyright
Other

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