02172nam 2200613I 450 991070577680332120170614162455.0(CKB)5470000002452636(OCoLC)990066147(EXLCZ)99547000000245263620170614d1996 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierTransonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method /John W. Edwards[Washington, DC] :[National Aeronautics and Space Administration],[1996]1 online resource (16 pages) illustrationsNASA-TM ;110484"EUROMECH-ColIoquium 349 Simulation of Fluid-Structure Interaction in Aeronautics, Gottingen, Germany, September 16-18, 1996."Includes bibliographical references (pages 15-16).Separated flownasatTransonic flownasatTransonic flutternasatTransonic speednasatUnsteady flownasatViscous flownasatComputational fluid dynamicsnasatCouplingnasatAirfoilsnasatMach numbernasatBoundary layer separationnasatAirfoil oscillationsnasatSeparated flow.Transonic flow.Transonic flutter.Transonic speed.Unsteady flow.Viscous flow.Computational fluid dynamics.Coupling.Airfoils.Mach number.Boundary layer separation.Airfoil oscillations.Edwards John W.684United States.National Aeronautics and Space Administration,GPOGPOBOOK9910705776803321Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method3533199UNINA