01992oam 2200553 450 991070581100332120170811100125.0(CKB)5470000002454311(OCoLC)858259381(EXLCZ)99547000000245431120130912j199810 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierImpingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel /Richard J. Re and Francis J. CaponeHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,October 1998.1 online resource (37 pages) illustrationsNASA/TM ;1998-208723"October 1998.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 7).Supersonic transportsnasatSupersonic speednasatStatic pressurenasatShock wavesnasatMach numbernasatBow wavesnasatBodies of revolutionnasatSupersonic transports.Supersonic speed.Static pressure.Shock waves.Mach number.Bow waves.Bodies of revolution.Re Richard J.1387323Capone Francis J.Langley Research Center,OCLCEOCLCEOCLCOOCLCQGPOBOOK9910705811003321Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel3437009UNINA