LEADER 02148nam  2200505I  450 
001 9910706575503321
005 20171120101354.0
035   $a(CKB)5470000002456690
035   $a(OCoLC)1012399577
035   $a(EXLCZ)995470000002456690
100   $a20171120j199908    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBlade heat transfer measurements and predictions in a transonic turbine cascade /$fP.W. Giel [and four others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center$cU.S. Army Research Laboratory,$dAugust 1999.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209296
225 1 $aARL-TR ;$v2029
300   $a"August 1999."
300   $a"Prepared for the 1999 International Gas Turbine and Aeroengine Congress cosponsored by the American Society of Mechanical Engineers and the International Gas Turbine Institute, Indianapolis, Indiana, June 7-10, 1999."
300   $a"Performing organization: NASA Glenn Research Center and U.S. Army Research Laboratory"--Report documentation page.
300   $aDescription based on online resource; title from PDF title page (NASA, viewed Nov. 20, 2017).
320   $aIncludes bibliographical references (pages 14-15).
606   $aHeat transfer$2nasat
606   $aHeat measurement$2nasat
606   $aSupersonic turbines$2nasat
606   $aRotor stator interactions$2nasat
606   $aRotor blades (turbomachinery)$2nasat
615  7$aHeat transfer.
615  7$aHeat measurement.
615  7$aSupersonic turbines.
615  7$aRotor stator interactions.
615  7$aRotor blades (turbomachinery)
700   $aGiel$b P. W$g(Paul W.),$01390071
712 02$aNASA Glenn Research Center,
712 02$aU.S. Army Research Laboratory.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706575503321
996   $aBlade heat transfer measurements and predictions in a transonic turbine cascade$93532497
997   $aUNINA