02266oam 2200601 450 991071387280332120200826120956.0(CKB)5470000002504964(OCoLC)1100474464(EXLCZ)99547000000250496420190508d1957 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90° /by Jim A. PenlandWashington, [D.C.] :National Advisory Committee for Aeronautics,1957.1 online resource (32 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 3861"January 1957.""Supersedes recently declassified NACA Research Memorandum L54A14 by Jim A. Penland, 1954"--Page 1.No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 13-14).Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to ninety degreesCylindersAerodynamicsAerodynamic loadWind tunnel testingHypersonic wind tunnelsAerodynamic loadfastCylindersAerodynamicsfastHypersonic wind tunnelsfastWind tunnel testingfastCylindersAerodynamics.Aerodynamic load.Wind tunnel testing.Hypersonic wind tunnels.Aerodynamic load.CylindersAerodynamics.Hypersonic wind tunnels.Wind tunnel testing.Penland Jim A.1416903United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOCOPTRAALGPOBOOK9910713872803321Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 903523799UNINA