Wind Tunnel Investigation of Pre-Production F/A-18E Lateral Characteristics Using Continuous Beta Sweep Test & Analysis Technique (CBSTAT)
Author:
Affiliation:
1. NAVAIR
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-5051
Reference12 articles.
1. BlueRibbonPanelIBriefing-F/A-18E/FUp/AutoWingDrop,Navy-BoeingCorrespondence,9-10 September 1997.
2. Hall,R.,andWoodson,S,"IntroductiontotheAbruptWingStall(AWS)Program,"AIAA-2003-0589, January2003.
3. McConnell, J. and Killingsworth, R. "Continuous Beta Sweep Test & Analysis Technique (CBSTAT) for PredictingWingDropBasedonStaticWindTunnelTesting,"AIAA-2004-5048,August2004.
4. Lamar, J., and Hall, R. "AWS Figure of Merit (FOM) Developed Parameters from Static, Transonic Model Tests,"AIAA-2003-0745,January2003.
5. 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.
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