Control surface interaction effects of the Active Aeroelastic Wing wind tunnel model
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American Institute of Aeronautics and Astronautics
Reference10 articles.
1. Boehm,B.,Flick,P.,Sanders,B.,Pettit,C.,Reichenbach,E.Y.,andZillmer,S."Staticaeroelasticresponse predictionsof theActiveAeroelastic Wing (AAW) flightresearch vehicle,"AIAA/ASME/ASCE/AHS/ASC Structures,StructuralDynamics andMaterials Conference,April2001,Seattle,Washington,AIAA-2001-1372.
2. Wieseman, C.D., Silva,W.A., Spain, C.V.,andHeeg,J."TransonicSmallDisturbanceandLinearAnalysis forthe ActiveAeroelasticWing Program,"46thAIAA/ASME/ASCE/AHS/ASCStructures,StructuralDynamicsand Materials Conference,April,2005,Austin,Texas.
3. Raveh, D.E., and Levy, Y. "CFD-Based Aeroelastic Response of an Active Aeroelastic Wing,"45thAIAA/ASME/ASCE/AHS/ASCStructures, Structural Dynamics and Materials Conference, April 2004,PalmSprings,California.AIAA2004-1515.
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