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035   $a(CKB)5470000002464442
035   $a(OCoLC)844683682
035   $a(EXLCZ)995470000002464442
100   $a20130526j199612    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of wake passing on turbine blade film cooling /$fJames David Heidmann
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dDecember 1996.
215   $a1 online resource (xvii, 248 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107380
300   $aTitle from title screen (viewed Aug. 3, 2016).
300   $a"December 1996."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 244-248).
606   $aTurbine blades$2nasat
606   $aFilm cooling$2nasat
606   $aWakes$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aTurbomachinery$2nasat
606   $aFlow distribution$2nasat
606   $aUnsteady aerodynamics$2nasat
615  7$aTurbine blades.
615  7$aFilm cooling.
615  7$aWakes.
615  7$aNavier-Stokes equation.
615  7$aComputational fluid dynamics.
615  7$aTurbomachinery.
615  7$aFlow distribution.
615  7$aUnsteady aerodynamics.
700   $aHeidmann$b James D.$01407008
712 02$aLewis Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707308103321
996   $aThe effect of wake passing on turbine blade film cooling$93487269
997   $aUNINA