01669nam 2200457I 450 991070372830332120150702141611.0(CKB)5470000002434440(OCoLC)912934667(EXLCZ)99547000000243444020150702j201410 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierConceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed /Daniel S. Jones [and four others]Edwards, CA :National Aeronautics and Space Administration, Armstrong Flight Research Center,October 2014.1 online resource (25 pages) color illustrationsNASA/TM ;2014-218376Title from title screen (viewed July 2, 2015)."October 2014."Includes bibliographical references (page 14).Convergent-divergent nozzlesnasatFlow distributionnasatInviscid flownasatNozzle designnasatRocket nozzlesnasatConvergent-divergent nozzles.Flow distribution.Inviscid flow.Nozzle design.Rocket nozzles.Jones Daniel S.1407604NASA Neil A. Armstrong Flight Research Center,GPOGPOBOOK9910703728303321Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed3536473UNINA