02209oam 2200601I 450 991071376260332120200729141810.0(CKB)5470000002504057(OCoLC)1100474463(EXLCZ)99547000000250405720190508d1949 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10⁶ to 9.0 x 10⁶ /by Laurence K. Loftin, Jr. and Hamilton A. SmithWashington, [D.C.] :National Advisory Committee for Aeronautics,1949.1 online resource (75 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 1945"October 1949."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 17).Aerodynamic characteristics of fifteen National Advisory Committee for Aeronautics airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)AerofoilsAerodynamicsReynolds numberAerodynamicsfastAerofoilsfastReynolds numberfastAerodynamic characteristicsnasatAirfoil profilesnasatAerofoils.Aerodynamics.Reynolds number.Aerodynamics.Aerofoils.Reynolds number.Aerodynamic characteristics.Airfoil profiles.Loftin Laurence K.1398356Smith Hamilton A.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910713762603321Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10⁶ to 9.0 x 10⁶3462005UNINA