Dynamic model testing of the X-31 configuration for high-angle-of-attack flight dynamics research

Author:

CROOM MARK1,FRATELLO DAVID1,WHIPPLE RAYMOND1,O'ROURKE MATTHEW2,TRILLING TODD2

Affiliation:

1. NASA, LangleyResearch Center, Hampton, VA

2. Lockheed Engineering & Sciences Co., Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. Roll 50% 70% -1-100%- damper I galn I I I I I I

Cited by 4 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. Overview of Dynamic Test Techniques for Flight Dynamics Research at NASA LaRC;25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2006-06-05

2. The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers;Progress in Aerospace Sciences;2003-02

3. Research on the F/A-18E/F using a 22 percent-dynamically-scaled drop model;Atmospheric Flight Mechanics Conference;2000-08-14

4. High-angle-of-attack yawing moment asymmetry of the X-31 aircraft from flight test;12th Applied Aerodynamics Conference;1994-06-20

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