02328oam 2200649I 450 991071388910332120200821132740.0(CKB)5470000002504799(OCoLC)1100474474(EXLCZ)99547000000250479920190508d1953 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierThe aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction /by Bennie W. Cocke, Jr., Marvin P. Fink, and Stanley M. GottliebWashington, [D.C.] :National Advisory Committee for Aeronautics,1953.1 online resource (63 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 2980"August 1953."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 14).AirplanesModelsWingsAerofoilsBoundary layer controlLift (Aerodynamics)Wind tunnel testingAerofoilsfastAirplanesModelsWingsfastBoundary layer controlfastLift (Aerodynamics)fastWind tunnel testingfastAirplanesModelsWings.Aerofoils.Boundary layer control.Lift (Aerodynamics)Wind tunnel testing.Aerofoils.AirplanesModelsWings.Boundary layer control.Lift (Aerodynamics)Wind tunnel testing.Cocke Bennie W.1401095Fink Marvin P.Gottlieb Stanley M.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910713889103321The aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction3469287UNINA