01918nam 2200517I 450 991070578960332120170612111142.0(CKB)5470000002452507(OCoLC)989874384(EXLCZ)99547000000245250720170612j201612 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierPassive rocket diffuser testing reacting flow performance of four second-throat geometries /Daniel R. Jones, Daniel C. Allgood, Grady P. Saunders[Stennis Space Center, Mississippi] :National Aeronautics and Space Administration, [Stennis Space Center],December 2016.1 online resource (26 pages) color illustrationsNASA technical memorandum ;2016-219221"December 2016.""The experimentation presented in this paper was carried out at SSC between May and August 2015" Page 3.Includes bibliographical references (pages 25-26).Passive rocket diffuser testing Boundary layer separationnasatComputational fluid dynamicsnasatFlow distributionnasatPressure effectsnasatPressure measurementnasatRocket enginesnasatBoundary layer separation.Computational fluid dynamics.Flow distribution.Pressure effects.Pressure measurement.Rocket engines.Jones Daniel R.1411498Allgood Daniel C.Saunders Grady P.John C. Stennis Space Center,GPOGPOBOOK9910705789603321Passive rocket diffuser testing3502901UNINA