01962nam 2200505I 450 991070791160332120170425082640.0(CKB)5470000002469457(OCoLC)973491864(EXLCZ)99547000000246945720170223j199611 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierInvestigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure /M. Moin Hussaini and John J. KorteHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,November 1996.1 online resource (12 pages) illustrationsNASA technical memorandum ;110295"November 1996.""Performing organization: NASA Langley Research Center" Report documentation page.Includes bibliographical references (pages 8-9).Investigation of low Reynolds number rocket nozzle design using parabolized Navier-Stokes based optimization procedureComputational fluid dynamicsnasatNavier-Stokes equationnasatNozzle designnasatRocket nozzlesnasatLow Reynolds numbernasatNozzle thrust coefficientsnasatComputational fluid dynamics.Navier-Stokes equation.Nozzle design.Rocket nozzles.Low Reynolds number.Nozzle thrust coefficients.Hussaini M. Moin1421953Korte John J.Langley Research Center,GPOGPOBOOK9910707911603321Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure3544802UNINA