02028oam 2200565I 450 991071376420332120200729110127.0(CKB)5470000002504040(OCoLC)1104148291(EXLCZ)99547000000250404020190610d1948 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8 /by W.F. Lindsey, D.B. Stevenson, and Bernard N. DaleyWashington, [D.C.] :National Advisory Committee for Aeronautics,1948.1 online resource (86 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 1546'September 1948."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 14).Aerodynamic characteristics of twenty four National Advisory Committee for Aeronautics 16-series airfoils at Mach numbers between 0.3 and 0.8AerodynamicsAerofoilsWind tunnel testingAerodynamicsfastAerofoilsfastWind tunnel testingfastAerodynamics.Aerofoils.Wind tunnel testing.Aerodynamics.Aerofoils.Wind tunnel testing.Lindsey W. F.1410527Daley Bernard N.Stevenson D. B.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910713764203321Aerodynamic characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.83499375UNINA