LEADER 02044nam  2200529Ia 450 
001 9910701129803321
005 20120109121940.0
035   $a(CKB)5470000002415752
035   $a(OCoLC)771927365
035   $a(EXLCZ)995470000002415752
100   $a20120109d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNumerical simulations of two-phase reacting flow in a single-element lean direct injection (LDI) combustor using NCC$b[electronic resource] /$fNan-Suey Liu, Tsan-Hsing Shih, C. Thomas Wey
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2011]
215   $a1 online resource (28 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2011-217031
300   $aTitle from title screen (viewed on Jan. 9, 2012).
300   $a"July 2011."
320   $aIncludes bibliographical references (pages 9-10).
517   $aNumerical simulations of two-phase reacting flow in a single-element lean direct injection 
606   $aInjection$2nasat
606   $aReacting flow$2nasat
606   $aTwo phase flow$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aDirect numerical simulation$2nasat
606   $aTurbulent combustion$2nasat
615  7$aInjection.
615  7$aReacting flow.
615  7$aTwo phase flow.
615  7$aComputational fluid dynamics.
615  7$aDirect numerical simulation.
615  7$aTurbulent combustion.
700   $aLiu$b Nan-Suey$01396999
701   $aShih$b Tsan-Hsing$f1940-$01396998
701   $aWey$b C. Thomas$01409246
712 02$aFundamental Aeronautics Program (U.S.)
712 02$aNASA Glenn Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701129803321
996   $aNumerical simulations of two-phase reacting flow in a single-element lean direct injection (LDI) combustor using NCC$93495132
997   $aUNINA