LEADER 02266oam 2200565I 450 001 9910706213703321 005 20240201224053.0 035 $a(CKB)5470000002456304 035 $a(OCoLC)227925158 035 $a(EXLCZ)995470000002456304 100 $a20080513j200001 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aExperimental heat transfer and bulk air temperature measurements for a multipass internal cooling model with ribs and bleed /$fDouglas Thurman, Philip Poinsatte 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center$cU.S. Army Research Laboratory,$dJanuary 2000. 215 $a1 online resource (13 pages) $cillustrations 225 1 $aNASA/TM ;$v2000-209772 300 $a"January 2000." 300 $a"Prepared for the 45th ASME International Gas Turbine Institute sponsored by the American Society of Mechanical Engineers, Munich, Germany, May 8-11, 2000." 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. 1, 2017). 300 $a"ARL-MR-471." 320 $aIncludes bibliographical references (pages 4-5). 606 $aHeat transfer$2nasat 606 $aTemperature measurement$2nasat 606 $aFilm cooling$2nasat 606 $aRibs (supports)$2nasat 606 $aTurbine blades$2nasat 606 $aBleeding$2nasat 615 7$aHeat transfer. 615 7$aTemperature measurement. 615 7$aFilm cooling. 615 7$aRibs (supports) 615 7$aTurbine blades. 615 7$aBleeding. 700 $aThurman$b Douglas R.$01391713 702 $aPoinsatte$b Philip E. 712 02$aNASA Glenn Research Center, 712 02$aU.S. Army Research Laboratory. 801 0$bDTICE 801 1$bDTICE 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910706213703321 996 $aExperimental heat transfer and bulk air temperature measurements for a multipass internal cooling model with ribs and bleed$93873410 997 $aUNINA