LEADER 01962nam  2200505I  450 
001 9910707911603321
005 20170425082640.0
035   $a(CKB)5470000002469457
035   $a(OCoLC)973491864
035   $a(EXLCZ)995470000002469457
100   $a20170223j199611    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aInvestigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure /$fM. Moin Hussaini and John J. Korte
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dNovember 1996.
215   $a1 online resource (12 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v110295
300   $a"November 1996."
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (pages 8-9).
517 3 $aInvestigation of low Reynolds number rocket nozzle design using parabolized Navier-Stokes based optimization procedure
606   $aComputational fluid dynamics$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aNozzle design$2nasat
606   $aRocket nozzles$2nasat
606   $aLow Reynolds number$2nasat
606   $aNozzle thrust coefficients$2nasat
615  7$aComputational fluid dynamics.
615  7$aNavier-Stokes equation.
615  7$aNozzle design.
615  7$aRocket nozzles.
615  7$aLow Reynolds number.
615  7$aNozzle thrust coefficients.
700   $aHussaini$b M. Moin$01421953
702   $aKorte$b John J.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707911603321
996   $aInvestigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure$93544802
997   $aUNINA