01537oam 2200457 450 991071591230332120210423131310.0(CKB)5470000002516976(OCoLC)1196870103(EXLCZ)99547000000251697620200922j196811 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffects of angle of attack and bluntness on the shock-layer properties of a 15°cone at Mach number of 10.6 /by Joseph W. ClearyWashington, D.C. :National Aeronautics and Space Administration,November 1968.1 online resource (38 pages) illustrationsNASA/TN ;D-4909"November 1968."Includes bibliographical references (page 11).Mach numbernasatAerodynamicsnasatConical shellsfastShock (Mechanics)fastMach number.Aerodynamics.Conical shells.Shock (Mechanics)Cleary Joseph W.1398111United States.National Aeronautics and Space Administration,COPCOPOCLCFOCLCOGPOBOOK9910715912303321Effects of angle of attack and bluntness on the shock-layer properties of a 15°cone at Mach number of 10.63460765UNINA