02045oam 2200613 450 991071655090332120210623132915.0(CKB)5470000002522647(OCoLC)20643001(OCoLC)760999383(OCoLC)867807810(EXLCZ)99547000000252264719891113j197212 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierTests of a mixed compression axisymmetric inlet with large transonic mass flow at Mach numbers 0.6 to 2.65 /by Donald B. Smeltzer and Norman E. SorensenWashington, D.C. :National Aeronautics and Space Administration,December 1972.1 online resource (v, 183 pages) illustrationsNASA/TN ;D-6971"December 1972."Includes bibliographical references (page 26).Jet enginesnasatMach numbernasatPropulsionnasatJet enginesAir intakesAerodynamics, TransonicAerodynamics, TransonicfastJet enginesAir intakesfastJet engines.Mach number.Propulsion.Jet enginesAir intakes.Aerodynamics, Transonic.Aerodynamics, Transonic.Jet enginesAir intakes.Smeltzer Donald B.1409446Sorensen Norman E.1930-United States.National Aeronautics and Space Administration,Ames Research Center.ABCABCOCLAD#OCLCEOCLCQOCLCOOCLCFOCLCQGPOBOOK9910716550903321Tests of a mixed compression axisymmetric inlet with large transonic mass flow at Mach numbers 0.6 to 2.653495893UNINA