High-angle-of-attack dynamic behavior of a model high-performance fighter aircraft-Reference-Cited by-同舟云学术

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High-angle-of-attack dynamic behavior of a model high-performance fighter aircraft

Published:1988-08-15 Issue: Volume: Page:
ISSN:
Container-title:15th Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

PLANEAUX JAMES¹,BARTH THOMAS²

Affiliation:

1. USAF, Institute of Technology, Wright-Patterson AFB, OH

2. USAF, Armament Laboratory, Eglin AFB, FL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-4368

Reference18 articles.

1. Hehra, R.K., and Carroll, J.V

2. negative rudder. 6e -15.71°,6a - 0.stable equilibria; unstable equilibria. I , / , I / I , / I , / , / , I ,/ , ( / , I , o -20.00 -10.00 0.00 10.00 2o.bo

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