LEADER 01895nam  2200493I  450 
001 9910702356003321
005 20121226161236.0
035   $a(CKB)5470000002426598
035   $a(OCoLC)822966252
035   $a(EXLCZ)995470000002426598
100   $a20121226d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLarge Eddy Simulation of a film cooling flow injected from an inclined discrete cylindrical hole into a crossflow with zero-pressure gradient turbulent boundary layer /$fPerry L. Johnson, Vikram Shyam
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012.
215   $a1 online resource (23 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217695
300   $aTitle from title screen (viewed on Dec. 26, 2012).
300   $a"August 2012."
320   $aIncludes bibliographical references (pages 22-23).
606   $aLarge eddy simulation$2nasat
606   $aFilm cooling$2nasat
606   $aPressure gradients$2nasat
606   $aReynolds averaging$2nasat
606   $aTurbulent mixing$2nasat
606   $aTurbulent boundary layer$2nasat
615  7$aLarge eddy simulation.
615  7$aFilm cooling.
615  7$aPressure gradients.
615  7$aReynolds averaging.
615  7$aTurbulent mixing.
615  7$aTurbulent boundary layer.
700   $aJohnson$b Perry L$01390438
701   $aShyam$b Vikram$01390439
712 02$aNASA Glenn Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702356003321
996   $aLarge Eddy Simulation of a film cooling flow injected from an inclined discrete cylindrical hole into a crossflow with zero-pressure gradient turbulent boundary layer$93443118
997   $aUNINA