02078oam 2200541 450 991070745500332120160819161243.0(CKB)5470000002464978(OCoLC)761330230(EXLCZ)99547000000246497820111115j198012 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierEffects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles /Jeffery A. Yetter, Laurance D. Leavitt[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,December 1980.1 online resource (116 pages) illustrationsNASA technical paper ;1771Title from title screen (viewed on Aug. 19, 2016)."December 1980.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 18-19).Convergent-divergent nozzlesnasatExhaust flow simulationnasatNozzle designnasatStatic pressurenasatWind tunnel testsnasatConvergent-divergent nozzles.Exhaust flow simulation.Nozzle design.Static pressure.Wind tunnel tests.Yetter Jeffery A.1419448Leavitt Laurence D.Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCOOCLCQGPOBOOK9910707455003321Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles3533934UNINA