02118oam 2200565I 450 991071388560332120200824130547.0(CKB)5470000002504834(OCoLC)1100474477(EXLCZ)99547000000250483420190508d1955 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 180° /by Chris C. Critzos, Harry H. Heyson, and Robert W. Boswinkle, JrWashington, [D.C.] :National Advisory Committee for Aeronautics,1955.1 online resource (21 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 3361"January 1955."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (pages 11-12).Aerodynamic characteristics of National Advisory Committee for Aeronautics 0012 airfoil section at angles of attack from 0 degrees to 180 degreesAerofoilsAngle of attack (Aerodynamics)Lift (Aerodynamics)AerofoilsfastAngle of attack (Aerodynamics)fastLift (Aerodynamics)fastAerofoils.Angle of attack (Aerodynamics)Lift (Aerodynamics)Aerofoils.Angle of attack (Aerodynamics)Lift (Aerodynamics)Critzos Chris C.1404415Heyson Harry H.Boswinkle Robert W.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910713885603321Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 1803478943UNINA