LEADER 02482nam 2200637 450 001 9910706550203321 005 20171201083621.0 035 $a(CKB)5470000002456946 035 $a(OCoLC)1013716494 035 $a(EXLCZ)995470000002456946 100 $a20171201j200106 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aDesign evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application /$fAli Abdul-Aziz, George Y. Baaklini, Ramakrishna T. Bhatt 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJune 2001. 215 $a1 online resource (15 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2001-210819 300 $a"June 2001." 300 $a"Prepared for the 103rd Annual Meeting and Exposition sponsored by The American Ceramic Society, Indianapolis, Indiana, April 22-25, 2001." 300 $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page. 320 $aIncludes bibliographical references (page 9). 606 $aSilicon nitrides$2nasat 606 $aFinite element method$2nasat 606 $aThermal stresses$2nasat 606 $aThermal environments$2nasat 606 $aHole geometry (mechanics)$2nasat 606 $aAir cooling$2nasat 606 $aThermodynamic efficiency$2nasat 606 $aCeramics$2nasat 606 $aTemperature distribution$2nasat 606 $aStress analysis$2nasat 606 $aCeramic coatings$2nasat 615 7$aSilicon nitrides. 615 7$aFinite element method. 615 7$aThermal stresses. 615 7$aThermal environments. 615 7$aHole geometry (mechanics) 615 7$aAir cooling. 615 7$aThermodynamic efficiency. 615 7$aCeramics. 615 7$aTemperature distribution. 615 7$aStress analysis. 615 7$aCeramic coatings. 700 $aAbdul-Aziz$b Ali$01395980 702 $aBaaklini$b George Y. 702 $aBhatt$b Ramakrishna T. 712 02$aNASA Glenn Research Center, 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910706550203321 996 $aDesign evaluation using finite element analysis of cooled silicon nitride plates for a turbine blade application$93455315 997 $aUNINA