LEADER 01847nam  2200493I  450 
001 9910707169303321
005 20160422151202.0
035   $a(CKB)5470000002461803
035   $a(OCoLC)947119580
035   $a(EXLCZ)995470000002461803
100   $a20160422j199511    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCalculations of diffuser flows with an anisotropic K-[epsilon] model /$f. Zhu and T.-H. Shih
210  1$aCleveland, Ohio :$cNational Aeronautics and Space AdministrationLewis Research Center,$dNovember 1995.
215   $a1 online resource (10 pages) $cillustrations
225 1 $aNASA contractor report ;$v198418
225 1 $aICOMP ;$vno. 95-21
300   $a"November 1995."
300   $a"Performing organization: Institute for Computational Mechanics in Propulsion, Cleveland, Ohio"--Report documentation page.
320   $aIncludes bibliographical references (page 6).
606   $aAxisymmetric flow$2nasat
606   $aIncompressible flow$2nasat
606   $aInternal flow$2nasat
606   $aK-epsilon turbulence model$2nasat
606   $aTurbulence effects$2nasat
615  7$aAxisymmetric flow.
615  7$aIncompressible flow.
615  7$aInternal flow.
615  7$aK-epsilon turbulence model.
615  7$aTurbulence effects.
700   $aZhu$b Jieping$01343642
702   $aShih$b Tsan-Hsing$f1940-
712 02$aLewis Research Center.$bInstitute for Computational Mechanics in Propulsion.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707169303321
996   $aCalculations of diffuser flows with an anisotropic K- model$93535958
997   $aUNINA