Flight test results of the F-16 aircraft modified with the axisymmetric vectoring exhaust nozzle

Author: Anna, Paul D.
Published: Jul 1, 1994.
Physical Description: 1 electronic document
Additional Creators: Kidman, David S.

Online Version

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Summary

The 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.

Other Subject(s)

AERODYNAMICS

Collection

NASA Technical Reports Server (NTRS) Collection.

Note

Document ID: 19950007831.
Accession ID: 95N14245.
NASA. Dryden Flight Research Center, Fourth High Alpha Conference, Volume 2; 15 p.

Terms of Use and Reproduction

No Copyright.

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