02088oam 2200577 450 991071513730332120201222122959.0(CKB)5470000002508643(OCoLC)937437996(EXLCZ)99547000000250864320160208d1931 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierExperiments with an airfoil model on which the boundary layer is controlled without the use of supplementary equipment /by I.H. AbbottWashington, [D.C.] :National Advisory Committee for Aeronautics,1931.1 online resource (6 pages, 5 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 371"April, 1931."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (pages 5-6).Boundary layer controlAerofoilsLeading edges (Aerodynamics)Lift (Aerodynamics)Angle of attack (Aerodynamics)Angle of attack (Aerodynamics)fastBoundary layer controlfastLift (Aerodynamics)fastBoundary layer control.Aerofoils.Leading edges (Aerodynamics)Lift (Aerodynamics)Angle of attack (Aerodynamics)Angle of attack (Aerodynamics)Boundary layer control.Lift (Aerodynamics)Abbott I. H.1398731United States.National Advisory Committee for Aeronautics,OCLCEOCLCEOCLCQOCLCFCOPGPOBOOK9910715137303321Experiments with an airfoil model on which the boundary layer is controlled without the use of supplementary equipment3462571UNINA