02020oam 2200589 450 991071608080332120210504105248.0(CKB)5470000002517294(OCoLC)150483928(OCoLC)761215476(EXLCZ)99547000000251729419871030j196901 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8 /by P. Calvin StainbackWashington, D.C. :National Aeronautics and Space Administration,January 1969.1 online resource (76 pages) illustrationsNASA/TN ;D-4961"January 1969."Includes bibliographical references (pages 24-27).Reynolds numbernasatAerodynamicsnasatMach numbernasatAerodynamics, HypersonicAerodynamics, HypersonicfastAngle of attack (Aerodynamics)fastNoses (Space vehicles)fastReynolds numberfastReynolds number.Aerodynamics.Mach number.Aerodynamics, Hypersonic.Aerodynamics, Hypersonic.Angle of attack (Aerodynamics)Noses (Space vehicles)Reynolds number.Stainback P. Calvin1401641United States.National Aeronautics and Space Administration,UAUUAUEGMAD#OCLCEOCLCFOCLCQGPOBOOK9910716080803321Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 83470598UNINA