01537nam 2200445 450 991070579400332120170609075749.0(CKB)5470000002452463(OCoLC)989724350(EXLCZ)99547000000245246320170609j201701 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierIncreased jet noise due to a "nominally laminar" state of nozzle exit boundary layer /K.B.M.Q. ZamanCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,January 2017.1 online resource (20 pages) color illustrationsNASA/TM ;2017-219440"January 2017."Includes bibliographical references (pages 8-9).Jet aircraft noisenasatJet nozzlesnasatSound pressurenasatSubsonic flownasatTurbulent boundary layernasatJet aircraft noise.Jet nozzles.Sound pressure.Subsonic flow.Turbulent boundary layer.Zaman K. B. M. Q(Khairul B. M. Q.),1392412NASA Glenn Research Center,GPOGPOBOOK9910705794003321Increased jet noise due to a "nominally laminar" state of nozzle exit boundary layer3462706UNINA