Dynamic model testing of the X-31 configuration for high-angle-of-attack flight dynamics research
Author:
Affiliation:
1. NASA, LangleyResearch Center, Hampton, VA
2. Lockheed Engineering & Sciences Co., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-3674
Reference14 articles.
1. Roll 50% 70% -1-100%- damper I galn I I I I I I
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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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