02350oam 2200601 450 991070731130332120160908121342.0(CKB)5470000002464409(OCoLC)844689779(EXLCZ)99547000000246440920130526j199611 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierThe effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct /Milo D. DahlCleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,November 1996.1 online resource (21 pages) illustrationsNASA technical memorandum ;107358Title from title screen (viewed Aug. 2, 2016)."November 1996"--Report documentation page."Prepared for the International Mechanical Engineering Congress and Exposition sponsored by the American Society of Mechanical Engineers, Atlanta, Georgia, November 17-22, 1996.""Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.Includes bibliographical references (pages 11-12).Supersonic jet flownasatDuctsnasatDucted flownasatDuct geometrynasatCircles (geometry)nasatBoundary conditionsnasatKelvin-Helmholtz instabilitynasatSupersonic inletsnasatSupersonic jet flow.Ducts.Ducted flow.Duct geometry.Circles (geometry)Boundary conditions.Kelvin-Helmholtz instability.Supersonic inlets.Dahl Milo D.1956-1397975Lewis Research Center,United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCOOCLCQGPOBOOK9910707311303321The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct3497084UNINA