LEADER 01491nam  2200445I  450 
001 9910707929203321
005 20170214102509.0
035   $a(CKB)5470000002469279
035   $a(OCoLC)972481340
035   $a(EXLCZ)995470000002469279
100   $a20170214j201610    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aIntegrated turbine tip clearance and gas turbine engine simulation /$fJeffryes W. Chapman [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dOctober 2016.
215   $a1 online resource (17 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2016-219146
300   $a"October 2016."
320   $aIncludes bibliographical references (page 17).
606   $aBlade tips$2nasat
606   $aGas turbine engines$2nasat
606   $aThermodynamics$2nasat
606   $aTurbine blades$2nasat
606   $aTurbocompressors$2nasat
615  7$aBlade tips.
615  7$aGas turbine engines.
615  7$aThermodynamics.
615  7$aTurbine blades.
615  7$aTurbocompressors.
700   $aChapman$b Jeffryes W.$01393596
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707929203321
996   $aIntegrated turbine tip clearance and gas turbine engine simulation$93525121
997   $aUNINA