LEADER 01616nam  2200457I  450 
001 9910713066703321
005 20200319134032.0
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035   $a(OCoLC)1145279742
035   $a(EXLCZ)995470000002499534
100   $a20200319j202003    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFuel flexible combustor for high-OPR compact-core N+3 propulsion engine $efinal technical report /$fLance L. Smith
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dMarch 2020.
215   $a1 online resource (91 pages) $cillustrations (mostly color)
225 1 $aNASA/CR ;$v2020-220489
300   $a"March 2020."
320   $aIncludes bibliographical references (page 91).
517   $aFuel flexible combustor for high-OPR compact-core N+3 propulsion engine 
606   $aBypass ratio$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aCombustion chambers$2nasat
606   $aHigh pressure$2nasat
606   $aDynamic tests$2nasat
615  7$aBypass ratio.
615  7$aComputational fluid dynamics.
615  7$aCombustion chambers.
615  7$aHigh pressure.
615  7$aDynamic tests.
700   $aSmith$b Lance L.$01394506
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910713066703321
996   $aFuel flexible combustor for high-OPR compact-core N+3 propulsion engine$93452010
997   $aUNINA