01776oam 2200481 450 991070997840332120180824073246.0(CKB)5470000002474480(OCoLC)1049569652(OCoLC)995470000002474480(EXLCZ)99547000000247448020180823j198502 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierStatic internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/Laurence D. LeavittWashington, D.C. :National Aeronautics and Space Administration, Scientific and Technical Information Branch,February 1985.1 online resource (66 pages) illustrationsNASA/TP ;2391"February 1985."Includes bibliographical references (pages 7-8).ConvergentnasatThrust vector controlnasatWind tunnel testsnasatNozzle flownasatTransonic wind tunnelsnasatConvergent.Thrust vector control.Wind tunnel tests.Nozzle flow.Transonic wind tunnels.Leavitt Laurence D.1394871United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,Langley Research Center.GPOGPOGPOBOOK9910709978403321Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊3452729UNINA