02041oam 2200553 450 991070745590332120160819145137.0(CKB)5470000002464969(OCoLC)785105971(EXLCZ)99547000000246496920120408j198012 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierInvestigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /Bobby L. Berrier and Richard J. Re[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,December 1980.1 online resource (215 pages) chiefly illustrationsNASA technical paper ;1766Title from title screen (viewed on Aug. 19, 2016)."December 1980.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 23).Convergent-divergent nozzlesnasatMach numbernasatNozzle designnasatPerformance testsnasatPressure rationasatConvergent-divergent nozzles.Mach number.Nozzle design.Performance tests.Pressure ratio.Berrier Bobby L.1389747Re Richard J.Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCFOCLCQOCLCOGPOBOOK9910707455903321Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft3545765UNINA