LEADER 02240oam  2200577I  450 
001 9910690371503321
005 20160809094929.0
035   $a(CKB)5470000002337576
035   $a(OCoLC)227848393
035   $a(EXLCZ)995470000002337576
100   $a20080512j199612    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEndwall heat transfer measurements in a transonic turbine cascade /$fP.W. Giel [and four others]
210  1$aCleveland, Ohio :$cNASA Lewis Research Center : U.S. Army Research Laboratory,$dDecember 1996.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107387
225 1 $aArmy Research Laboratory technical report ;$vARL-TR-1253
300   $aTitle from title screen (viewed Aug. 9, 2016).
300   $a"December 1996"--Report documentation page.
300   $a"Prepared for the 41st Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Birmingham, United Kingdom, June 10-13, 1996."
300   $a"Performing organization: NASA Lewis Research Center and U.S. Army Research Laboratory"--Report documentation page.
320   $aIncludes bibliographical references (pages 14-15).
606   $aHeat transfer$2nasat
606   $aTurbine blades$2nasat
606   $aTurbulent flow$2nasat
606   $aFlow distribution$2nasat
606   $aSupersonic turbines$2nasat
606   $aWall flow$2nasat
606   $aCascade wind tunnels$2nasat
615  7$aHeat transfer.
615  7$aTurbine blades.
615  7$aTurbulent flow.
615  7$aFlow distribution.
615  7$aSupersonic turbines.
615  7$aWall flow.
615  7$aCascade wind tunnels.
700   $aGiel$b P. W$g(Paul W.),$01390071
712 02$aLewis Research Center,
712 02$aU.S. Army Research Laboratory,
801  0$bDTICE
801  1$bDTICE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910690371503321
996   $aEndwall heat transfer measurements in a transonic turbine cascade$93530572
997   $aUNINA