Impact of nose-probe chines on the vortex flows about the F-16C
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton,VA
2. George Washington University, Hampton, VA
3. General Dynamics Corp., Fort Worth, TX
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-386
Reference13 articles.
1. Experimental investigation of the F/A-18 vortex flows at subsonic through transonic speeds
2. Flow studies of slender wing vortices
3. Observation of airplane flowfields by natural condensation effects
Cited by 6 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. Two-dimensional vortex motion in the cross-flow of a wing-body configuration;Journal of Fluid Mechanics;1995-12-25
2. Secondary flow control on slender, sharp-edged configurations;11th Applied Aerodynamics Conference;1993-08-09
3. Forebody vortex control with miniature, rotatable nose-boom strakes;30th Aerospace Sciences Meeting and Exhibit;1992-01-06
4. The dynamic character of the wake of an axisymmetric body at an angle of attack;9th Applied Aerodynamics Conference;1991-08-17
5. Aerodynamic control using forebody strakes;29th Aerospace Sciences Meeting;1991-01-07
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