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High-Order Space-Time Methods for Conservation LawsCurrent high-order methods such as discontinuous Galerkin and/or flux reconstruction can provide effective discretization for the spatial derivatives. Together with a time discretization, such methods result in either too small a time step size in the case of an explicit scheme or a very large system in the case of an implicit one. To tackle these problems, two new high-order space-time schemes for conservation laws are introduced: the first is explicit and the second, implicit. The explicit method here, also called the moment scheme, achieves a Courant-Friedrichs-Lewy (CFL) condition of 1 for the case of one-spatial dimension regardless of the degree of the polynomial approximation. (For standard explicit methods, if the spatial approximation is of degree p, then the time step sizes are typically proportional to 1/p(exp 2)). Fourier analyses for the one and two-dimensional cases are carried out. The property of super accuracy (or super convergence) is discussed. The implicit method is a simplified but optimal version of the discontinuous Galerkin scheme applied to time. It reduces to a collocation implicit Runge-Kutta (RK) method for ordinary differential equations (ODE) called Radau IIA. The explicit and implicit schemes are closely related since they employ the same intermediate time levels, and the former can serve as a key building block in an iterative procedure for the latter. A limiting technique for the piecewise linear scheme is also discussed. The technique can suppress oscillations near a discontinuity while preserving accuracy near extrema. Preliminary numerical results are shown
Document ID
20140002885
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Huynh, H. T.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
April 11, 2014
Publication Date
September 1, 2013
Subject Category
Aeronautics (General)
Numerical Analysis
Report/Patent Number
E-18759
AIAA Paper 2013-2432
NASA/TM-2013-218077
Meeting Information
Meeting: Computational Fluid Dynamics Conference
Location: San Diego, CA
Country: United States
Start Date: June 24, 2013
End Date: June 27, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 794072.02.03.02.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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