LEADER 01800nam  2200469I  450 
001 9910705810803321
005 20170811105536.0
035   $a(CKB)5470000002454313
035   $a(OCoLC)1000386845
035   $a(EXLCZ)995470000002454313
100   $a20170811j201707    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAxial-flow turbine rotor discharge-flow overexpansion and limit-loading condition$hpart 1$iComputational fluid dynamics (CFD) investigation /$fShu-Cheng S. Chen
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJuly 2017.
215   $a1 online resource (iii, 37 pages)
225 1 $aNASA/TM ;$v2017-219506
300   $a"July 2017."
320   $aIncludes bibliographical references (page 37).
327   $apt. 1. Computational fluid dynamics (CFD) investigation.
517   $aAxial-flow turbine rotor discharge-flow overexpansion and limit-loading condition. part 1, Computational fluid dynamics 
606   $aComputational fluid dynamics$2nasat
606   $aAxial flow turbines$2nasat
606   $aTurbine blades. formula$2nasat
606   $aSupercritical flow$2nasat
606   $aCritical flow$2nasat
615  7$aComputational fluid dynamics.
615  7$aAxial flow turbines.
615  7$aTurbine blades. formula.
615  7$aSupercritical flow.
615  7$aCritical flow.
700   $aChen$b Shu-Cheng S.$01410451
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705810803321
996   $aAxial-flow turbine rotor discharge-flow overexpansion and limit-loading condition$93516729
997   $aUNINA