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100   $a20140916j197302    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSimultaneous film and convection cooling of a plate inserted in the exhaust stream of a gas turbine combustor /$fby Cecil J. Marek and Albert J. Juhasz
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dFebruary 1973.
215   $a1 online resource (iii, 34 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7156
300   $a"February 1973."
320   $aIncludes bibliographical references (page 34).
606   $aGas turbines$2nasat
606   $aCombustion chambers$2nasat
606   $aGas-turbines$xCombustion
606   $aCombustion chambers$xMaterials$xCooling
606   $aGas-turbines$xCombustion$2fast
615  7$aGas turbines.
615  7$aCombustion chambers.
615  0$aGas-turbines$xCombustion.
615  0$aCombustion chambers$xMaterials$xCooling.
615  7$aGas-turbines$xCombustion.
700   $aMarek$b Cecil J.$01399045
702   $aJuhasz$b Albert J.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLewis Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bABC
801  2$bAD#
801  2$bOCLCQ
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910716669203321
996   $aSimultaneous film and convection cooling of a plate inserted in the exhaust stream of a gas turbine combustor$93463661
997   $aUNINA