Wind tunnel evaluation of tactical aircraft stability and control asaffected by nozzle thrust reverser parameter variations
Author:
Affiliation:
1. Northrop Corp., Aircraft Div., Hawthorne, CA
2. USAF, Flight Dynamics Laboratory, Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1228
Reference5 articles.
1. Effect of in-flight thrust reverser deployment on tactical aircraft stability and control
2. Glezer, A, Hughes, R.V., and Hunt, B.I. "Thrust Reverser Effects on the Tail Surface Aerodynamics of an F-18 Type Configuration." AIAA-83-1860.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Fluidic scale model multi-plane thrust vector control test results;29th Joint Propulsion Conference and Exhibit;1993-06-28
2. Thrust reverser effects on the tail surface aerodynamics of an F-18 type configuration;Applied Aerodynamics Conference;1983-07-13
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