Fluidic scale model multi-plane thrust vector control test results
Author:
Affiliation:
1. Rohr, Inc., Chula Vista, CA
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-2433
Reference16 articles.
1. Richey, G.K., Bemer, B.L., Palcza, J.L. "Two-Dimensional NozzldAirframe Integration Technology -AnOverview,"AIMPaper 77-839, July 1977
2. ItisforReal,"AIAAPaper 79-1810, August 1979
3. ./ Flight Thrust Reverser," AIAA Paper 74-1170 October 1974
4. Chiarelli, C., Compton,M. Lt. "WindTunnel Evaluationof TacticalAircraft Stabilityand Control as Affected By Nozzle Thrust Reverser Parameter Variations,"AIAAPaper 83-11228,June 1983
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