02746oam 2200697I 450 991071375710332120200730140530.0(CKB)5470000002504112(OCoLC)1100474462(EXLCZ)99547000000250411220190508d1950 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section /by Hamilton A. Smith and Raymond F. SchaeferWashington, [D.C.] :National Advisory Committee for Aeronautics,1950.1 online resource (18 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 2074"April 1950."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 9).Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the National Advisory Committee for Aeronautics 0012 airfoil sectionAerofoilsAerodynamicsLift (Aerodynamics)Drag (Aerodynamics)Pitching (Aerodynamics)Reynolds numberAerodynamicsfastAerofoilsfastDrag (Aerodynamics)fastLift (Aerodynamics)fastPitching (Aerodynamics)fastReynolds numberfastAerofoils.Aerodynamics.Lift (Aerodynamics)Drag (Aerodynamics)Pitching (Aerodynamics)Reynolds number.Aerodynamics.Aerofoils.Drag (Aerodynamics)Lift (Aerodynamics)Pitching (Aerodynamics)Reynolds number.Smith Hamilton A.1401175Schaefer Raymond F.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910713757103321Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section3469532UNINA