LEADER 01669nam  2200457I  450 
001 9910703728303321
005 20150702141611.0
035   $a(CKB)5470000002434440
035   $a(OCoLC)912934667
035   $a(EXLCZ)995470000002434440
100   $a20150702j201410    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aConceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed /$fDaniel S. Jones [and four others]
210  1$aEdwards, CA :$cNational Aeronautics and Space Administration, Armstrong Flight Research Center,$dOctober 2014.
215   $a1 online resource (25 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218376
300   $aTitle from title screen (viewed July 2, 2015).
300   $a"October 2014."
320   $aIncludes bibliographical references (page 14).
606   $aConvergent-divergent nozzles$2nasat
606   $aFlow distribution$2nasat
606   $aInviscid flow$2nasat
606   $aNozzle design$2nasat
606   $aRocket nozzles$2nasat
615  7$aConvergent-divergent nozzles.
615  7$aFlow distribution.
615  7$aInviscid flow.
615  7$aNozzle design.
615  7$aRocket nozzles.
700   $aJones$b Daniel S.$01407604
712 02$aNASA Neil A. Armstrong Flight Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703728303321
996   $aConceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed$93536473
997   $aUNINA