BEGIN:VCALENDAR VERSION:2.0 PRODID:-//ÎçÒ¹¾ç³¡ - ECPv6.15.15//NONSGML v1.0//EN CALSCALE:GREGORIAN METHOD:PUBLISH X-ORIGINAL-URL: X-WR-CALDESC:Events for ÎçÒ¹¾ç³¡ REFRESH-INTERVAL;VALUE=DURATION:PT1H X-Robots-Tag:noindex X-PUBLISHED-TTL:PT1H BEGIN:VTIMEZONE TZID:America/Los_Angeles BEGIN:DAYLIGHT TZOFFSETFROM:-0800 TZOFFSETTO:-0700 TZNAME:PDT DTSTART:20180311T100000 END:DAYLIGHT BEGIN:STANDARD TZOFFSETFROM:-0700 TZOFFSETTO:-0800 TZNAME:PST DTSTART:20181104T090000 END:STANDARD BEGIN:DAYLIGHT TZOFFSETFROM:-0800 TZOFFSETTO:-0700 TZNAME:PDT DTSTART:20190310T100000 END:DAYLIGHT BEGIN:STANDARD TZOFFSETFROM:-0700 TZOFFSETTO:-0800 TZNAME:PST DTSTART:20191103T090000 END:STANDARD BEGIN:DAYLIGHT TZOFFSETFROM:-0800 TZOFFSETTO:-0700 TZNAME:PDT DTSTART:20200308T100000 END:DAYLIGHT BEGIN:STANDARD TZOFFSETFROM:-0700 TZOFFSETTO:-0800 TZNAME:PST DTSTART:20201101T090000 END:STANDARD END:VTIMEZONE BEGIN:VEVENT DTSTART;TZID=America/Los_Angeles:20190301T121000 DTEND;TZID=America/Los_Angeles:20190301T130000 DTSTAMP:20260611T163306 CREATED:20190226T215531Z LAST-MODIFIED:20190226T215639Z UID:64409-1551442200-1551445200@tricities.wsu.edu SUMMARY:MME Seminar Series: The Dynamics and Thermodynamics of Gas Dynamic Shock Waves DESCRIPTION:This seminar presents a computational investigation of shock-wave structures through a novel\nimplicit high-order Galerkin finite element Runge–Kutta algorithm. The algorithm induces no spatial\ndiscretization artificial diffusion\, relies on cubic and higher-degree elements for an accurate resolution\nof the steep shock gradients\, uses an implicit time integration for swift convergence to steady states\,\nand employs original Neumann-type outlet boundary conditions in the form of generalized Rankine\nHugoniot conditions on normal stress and balance of heat flux and deviatoric-stress work per unit time.\nThrough an innovative approach\, the formulation also calculates the shock extent\, which is an additional\nunknown\, and employs the single non dimensional (0\, 1) computational domain for the determination\nof any shock structure. The algorithm rapidly generates steady shock structures\, in at most 150 time\nsteps for any upstream Mach number considered in this study\, in the range 1.05 < M < 10.0. The finite\nelement discretization is shown to be asymptotically convergent under progressive grid refinements\, in\nrespect of both the H0 and H1 error norms\, with an H0 accuracy order as high as 6 and reduction of the\ndiscretization error to the round-off-error threshold of 1 x10-9 with just 420 computational cells and\n5th-degree elements. For any upstream Mach number\, the computational results are shown to satisfy the\nRankine–Hugoniot conditions\, an established requirement for solution reliability. \nMME Seminar_Flyer_Iannelli_03.01.2019 \n  URL:/event/mme-seminar-series-the-dynamics-and-thermodynamics-of-gas-dynamic-shock-waves/ LOCATION:BSEL 102 CATEGORIES:academic,Calendar,student,university ORGANIZER;CN="Changki Mo":MAILTO:changki.mo@wsu.edu END:VEVENT END:VCALENDAR