02068oam 2200589 450 991070743880332120160825114551.0(CKB)5470000002465142(OCoLC)761383274(EXLCZ)99547000000246514220111115j198012 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierA study of the sonic-boom characteristics of a blunt body at a Mach number of 6 /George C. Ashby, Jr[Washington, D.C.] :National Aeronautics and Space Administration, Scientific and Technical Information Branch,December 1980.1 online resource (31 pages) illustrationsNASA technical paper ;1787Title from title screen (viewed on Aug. 23, 2016)."December 1980.""Performing Organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (page 9).Blunt bodiesnasatFar fieldsnasatFinite difference theorynasatSonic boomsnasatStatic pressurenasatAerodynamics, SupersonicfastSonic boomfastBlunt bodies.Far fields.Finite difference theory.Sonic booms.Static pressure.Aerodynamics, Supersonic.Sonic boom.Ashby George C.196768Langley Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Branch,OCLCEOCLCEOCLCQOCLCFOCLCOOCLCQGPOBOOK9910707438803321A study of the sonic-boom characteristics of a blunt body at a Mach number of 63434677UNINA