LEADER 01586nam  2200481   450 
001 9910709984303321
005 20180822083018.0
035   $a(CKB)5470000002474420
035   $a(OCoLC)1049172071
035   $a(EXLCZ)995470000002474420
100   $a20180822j198206    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aHigh pressure turbine test hardware detailed design report /$fE.E. Halila, D.T. Lenahan, T.T. Thomas
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJune 1982.
215   $a1 online resource (ix, 186 pages) $cillustrations
225 1 $aNASA/CR ;$v167355
300   $a"June 1982."
320   $aIncludes bibliographical references (page 181).
517 1 $aEnergy efficient engine
606   $aAircraft engines$2nasat
606   $aTurbine blades$2nasat
606   $aHigh pressure$2nasat
606   $aEnergy conversion efficiency$2nasat
606   $aFlow distribution$2nasat
615  7$aAircraft engines.
615  7$aTurbine blades.
615  7$aHigh pressure.
615  7$aEnergy conversion efficiency.
615  7$aFlow distribution.
700   $aHalila$b E. E.$01388311
702   $aLenahan$b D. T.
702   $aThomas$b T. T.
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910709984303321
996   $aHigh pressure turbine test hardware detailed design report$93438802
997   $aUNINA