LEADER 02127oam  2200625   450 
001 9910716643603321
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035   $a(OCoLC)995470000002523730
035   $a(EXLCZ)995470000002523730
100   $a20111115j197506    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMetal temperatures and coolant flow in a wire-cloth transpiration-cooled turbine vane /$fHerbert J. Gladden
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dJune 1975.
215   $a1 online resource (22 pages) $cillustrations
225 1 $aNASA/TM ;$vX-3248
300   $a"June 1975."
320   $aIncludes bibliographical references (pages 10-11).
606   $aGas turbines$2nasat
606   $aGas turbine engines$2nasat
606   $aHeat transfer$2nasat
606   $aAircraft gas-turbines$xBlades$xCooling
606   $aAircraft gas-turbines$xBlades$xMaterials$xEffect of temperature on
606   $aHeat$xTransmission
606   $aAircraft gas-turbines$xBlades$xCooling$2fast
606   $aHeat$xTransmission$2fast
615  7$aGas turbines.
615  7$aGas turbine engines.
615  7$aHeat transfer.
615  0$aAircraft gas-turbines$xBlades$xCooling.
615  0$aAircraft gas-turbines$xBlades$xMaterials$xEffect of temperature on.
615  0$aHeat$xTransmission.
615  7$aAircraft gas-turbines$xBlades$xCooling.
615  7$aHeat$xTransmission.
700   $aGladden$b Herbert J.$01386769
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bGPO
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910716643603321
996   $aMetal temperatures and coolant flow in a wire-cloth transpiration-cooled turbine vane$93550419
997   $aUNINA