LEADER 01595nam  2200481   450 
001 9910709984203321
005 20180822090408.0
035   $a(CKB)5470000002474421
035   $a(OCoLC)1049172179
035   $a(EXLCZ)995470000002474421
100   $a20180822j198208    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLow pressure turbine test hardware detailed design report /$fD.G. Cherry, C.H. Gay, D.T. Lenahan
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dAugust 1982.
215   $a1 online resource (xiii, 173 pages) $cillustrations
225 1 $aNASA/CR ;$v167956
300   $a"August 1982."
517 1 $aEnergy efficient engine
606   $aAircraft engines$2nasat
606   $aLow pressure$2nasat
606   $aTurbine blades$2nasat
606   $aEngine design$2nasat
606   $aACEE program$2nasat
615  7$aAircraft engines.
615  7$aLow pressure.
615  7$aTurbine blades.
615  7$aEngine design.
615  7$aACEE program.
700   $aCherry$b D. G.$01415822
702   $aGay$b C. H.
702   $aLenahan$b D. T.
712 02$aLewis Research Center,
712 02$aGeneral Electric Company.$bAircraft Engine Business Group.$bAdvanced Technology Programs Department.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910709984203321
996   $aLow pressure turbine test hardware detailed design report$93518929
997   $aUNINA