01817oam 2200529 450 991071597010332120210402140027.0(CKB)5470000002516392(OCoLC)760927075(EXLCZ)99547000000251639220111114j196808 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierCalibration of 30° included-angle cone for determining local flow conditions in Mach number range of 1.51 to 3.51 /Walter A. Vahl and Robert L. WeirichWashington, D.C. :National Aeronautics and Space Administration,August 1968.1 online resource (39 pages) illustrationsNASA/TN ;D-4679"August 1968."Includes bibliographical references (page 11).Base flownasatSupersonic transportsnasatBase flow (Aerodynamics)fastConeAerodynamicsfastMach numberfastSupersonic transport planesfastBase flow.Supersonic transports.Base flow (Aerodynamics)ConeAerodynamics.Mach number.Supersonic transport planes.Vahl Walter A.1410462Weirich Robert L.United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCFOCLCQGPOBOOK9910715970103321Calibration of 30° included-angle cone for determining local flow conditions in Mach number range of 1.51 to 3.513499148UNINA