Overview of Dynamic Test Techniques for Flight Dynamics Research at NASA LaRC-Reference-Cited by-同舟云学术

Overview of Dynamic Test Techniques for Flight Dynamics Research at NASA LaRC

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
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Author:

Owens Bruce¹,Brandon Jay¹,Croom Mark¹,Fremaux Mike¹,Heim Gene¹,Vicroy Dan¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3146

Reference37 articles.

1. Research on the F/A-18E/F using a 22 percent-dynamically-scaled drop model

2. 3Croom, M.A., Fratello, D.J., Whipple, R.D., O'Rourke, M.J., and Trilling, T.W. "Dynamic Model Testing Of The X-31Configuration ForHigh-Angle-of-Attack,"AIAA93-3674-CP,August1993.

3. 5Wolowicz,Chester,H.;Bowman,James,S.;andGilbert,William,P.:SimilitudeRequirementsandScaling Relationships asApplied toModelTesting. NASATP-1435,August1979.

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