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101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAnalysis of turbine blade relative cooling flow factor used in the subroutine coolit based on film cooling correlations /$fSteven J. Schneider
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJune 2015.
215   $a1 online resource (24 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218738
300   $aTitle from title screen (viewed on Aug. 18, 2015).
300   $a"June 2015."
320   $aIncludes bibliographical references (page 24).
606   $aTurbine blades$2nasat
606   $aFilm cooling$2nasat
606   $aFlat plates$2nasat
606   $aTurbulent heat transfer$2nasat
606   $aConvection$2nasat
615  7$aTurbine blades.
615  7$aFilm cooling.
615  7$aFlat plates.
615  7$aTurbulent heat transfer.
615  7$aConvection.
700   $aSchneider$b Steven J.$0248818
702   $aIshac$b Joseph
702   $aShalkhauser$b Kurt A.
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703824403321
996   $aAnalysis of turbine blade relative cooling flow factor used in the subroutine coolit based on film cooling correlations$93442243
997   $aUNINA

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