LEADER 01580oam  2200457   450 
001 9910716971303321
005 20211103131201.0
035   $a(CKB)5470000002526481
035   $a(OCoLC)1282246460
035   $a(OCoLC)995470000002526481
035   $a(EXLCZ)995470000002526481
100   $a20211103j196904    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSensitivity of subsonic transport range to turbofan engine design /$fby Robert W. Koenig and Laurence H. Fishbach
210  1$a[Washington, D.C] :$cNational Aeronautics and Space Administration,$dApril 1969.
215   $a1 online resource (approximately 20 pages) $cillustrations
225 1 $aNASA/TM ;$vX-52603
300   $a"April 1969."
320   $aIncludes bibliographical references (page 10).
606   $aTurbofan engines$2nasat
606   $aSubsonic flow$2nasat
606   $aDescent propulsion systems$2nasat
606   $aAscent propulsion systems$2nasat
615  7$aTurbofan engines.
615  7$aSubsonic flow.
615  7$aDescent propulsion systems.
615  7$aAscent propulsion systems.
700   $aKoenig$b Robert W.$01406898
702   $aFishbach$b Laurence H.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910716971303321
996   $aSensitivity of subsonic transport range to turbofan engine design$93513042
997   $aUNINA