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High angle-of-attack characteristics of a forward-swept wing fighter configurationThe NASA-Langley Research Center is currently investigating the high angle-of-attack characteristics of a forward-swept wing fighter technology demonstrator in a cooperative program with the Defense Advanced Research Projects Agency. The program includes static and dynamic wind-tunnel force tests, free-flight model tests, spin-tunnel tests, and piloted simulation. Particular emphasis is placed on identifying the contributions of the forward-swept wing to the configuration aerodynamics at high angles of attack. Results are presented to illustrate the wing contributions in terms of aerodynamic stability, flow visualization, and observation of free-flight characteristics.
Document ID
19820055564
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Grafton, S. B.
(NASA Langley Research Center Hampton, VA, United States)
Gilber, W. P.
(NASA Langley Research Center Hampton, VA, United States)
Croom, M. A.
(NASA Langley Research Center Hampton, VA, United States)
Murri, D. G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1982
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 82-1322
Report Number: AIAA PAPER 82-1322
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference
Location: San Diego, CA
Start Date: August 9, 1982
End Date: August 11, 1982
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82A39099
Distribution Limits
Public
Copyright
Other

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