02141nam 2200517 450 991070797090332120170126102049.0(CKB)5470000002468858(OCoLC)970166733(EXLCZ)99547000000246885820170126j198410 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierStatic internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° /Bobby L. Berrier and Laurence D. Leavitt[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,October 1984.1 online resource (141 pages) illustrationsNASA technical paper ;2364"October 1984" Report documentation page."Performing organization: NASA Langley Research Center" Report documentation page.Includes bibliographical references (page 11).Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60 degreesAxisymmetric bodiesnasatNozzle thrust coefficientsnasatStatic testsnasatThrust vector controlnasatTransonic wind tunnelsnasatTwo dimensional flownasatAxisymmetric bodies.Nozzle thrust coefficients.Static tests.Thrust vector control.Transonic wind tunnels.Two dimensional flow.Berrier Bobby L.1389747Leavitt Laurence D.Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,GPOGPOBOOK9910707970903321Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 603514191UNINA