02201oam 2200637 450 991071501640332120201130145740.0(CKB)5470000002507844(OCoLC)1100474485(EXLCZ)99547000000250784420190508d1950 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7 /by M. J. Turner and S. RabinowitzWashington, [D.C.] :National Advisory Committee for Aeronautics,1950.1 online resource (46 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 2213"October 1950"No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 19).AerofoilsFlaps (Airplanes)Lift (Aerodynamics)Pitching (Aerodynamics)Hinge moments (Aerodynamics)AerofoilsfastFlaps (Airplanes)fastHinge moments (Aerodynamics)fastLift (Aerodynamics)fastPitching (Aerodynamics)fastAerofoils.Flaps (Airplanes)Lift (Aerodynamics)Pitching (Aerodynamics)Hinge moments (Aerodynamics)Aerofoils.Flaps (Airplanes)Hinge moments (Aerodynamics)Lift (Aerodynamics)Pitching (Aerodynamics)Turner M. J.1404882Rabinowitz S.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910715016403321Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.73480367UNINA