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Flight test results of the F-16 aircraft modified with the axisymmetric vectoring exhaust nozzleThe results of the envelope expansion phase of the F-16 Multi-Axis Thrust Vectoring (MATV) program are presented in viewgraph format. The objectives and test approach are presented followed by results of testing with the initial control law configuration. The revised flight control laws are discussed followed by test results with the revised control laws. Additional testing added to the program, nose chines, parameter identification maneuvers, and the extended range angle of attack cones are briefly discussed.
Document ID
19950007831
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anna, Paul D. (Lockheed Corp. Fort Worth, TX, United States)
Kidman, David S. (Lockheed Corp. Fort Worth, TX, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Publication Information
Publication: NASA. Dryden Flight Research Center, Fourth High Alpha Conference, Volume 2
Subject Category
Aerodynamics
Accession Number
95N14245
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19950007815Collected WorksFourth High Alpha Conference: Volume 1
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