01714oam 2200529 450 991071657120332120210614094037.0(CKB)5470000002522442(OCoLC)785167531(EXLCZ)99547000000252244220120408j197210 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierExperimental study of nozzle wall boundary layers at Mach numbers 20 to 47 /by Joseph H. Kemp and F. Kevin OwenWashington, D.C. :National Aeronautics and Space Administration,October 1972.1 online resource (vii, 101 pages) illustrationsNASA/TN ;D-6965"October 1972."Includes bibliographical references (pages 17-21).Jet nozzlesnasatTurbulent boundary layernasatWall pressurenasatWall pressure (Aerodynamics)Aerodynamics, HypersonicJet nozzles.Turbulent boundary layer.Wall pressure.Wall pressure (Aerodynamics)Aerodynamics, Hypersonic.Kemp Joseph H.1402441Owen F. KevinUnited States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCOOCLCQCOPOCLCOGPOBOOK9910716571203321Experimental study of nozzle wall boundary layers at Mach numbers 20 to 473472911UNINA