Correlation of the Continuous Beta Sweep Test and Analysis Technique to Transonic Free-to-Roll and Flight Test Results-Reference-Cited by-同舟云学术

Correlation of the Continuous Beta Sweep Test and Analysis Technique to Transonic Free-to-Roll and Flight Test Results

Published:2004-06-22 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
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Author:

Cook Stephen¹,Ghee Terence¹,Gonzalez Hugo¹,Kokolios Alexander¹,Pettersson Henrik¹,Owens D.²

Affiliation:

1. NAVAIR

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-5052

Reference10 articles.

1. Chambers, J. and Hall, R. "Historical Review of Uncommanded Lateral-Directional Motions at Transonic Conditions(Invited),"AIAA-2003-0590,January2003.

2. Traven,R.,Hagan,J.andNiewoehner,R."SolvingWingdropontheF/A-18E/FSuperHornet,"1998Report to theAerospace Profession,Society of ExperimentalTest Pilots, September1998,pp.67-84.

3. Owens, B., Brandon, J., Hall, R., and Cunningham, K. "Free-To-Roll Analysis of Abrupt Wing Stall on Military Aircraft at TransonicSpeeds,"AIAA-2003-0750,January2003.

4. Lamar, J., and Hall, R. "AWS Figure of Merit (FOM) Developed Parameters from Static, Transonic Model Tests,"AIAA-2003-0745,January2003.

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