02165oam 2200589 450 991071388730332120200824092530.0(CKB)5470000002504817(OCoLC)1100474482(EXLCZ)99547000000250481720190508d1954 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10⁶ to 8.0 x 10⁶ /by Laurence K. Loftin, JrWashington, [D.C.] :National Advisory Committee for Aeronautics,1954.1 online resource (17 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 3244"August 1954."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 5).Aerodynamic characteristics of the National Advisory Committee for Aeronautics 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6)AerofoilsAerodynamicsMach numberReynolds numberAerodynamicsfastAerofoilsfastMach numberfastReynolds numberfastAerofoils.Aerodynamics.Mach number.Reynolds number.Aerodynamics.Aerofoils.Mach number.Reynolds number.Loftin Laurence K.1398356United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910713887303321Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 403522372UNINA