2007
DOI: 10.1016/j.jcp.2007.02.023
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Accurate monotonicity- and extrema-preserving methods through adaptive nonlinear hybridizations

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Cited by 68 publications
(76 citation statements)
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References 42 publications
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“…In our computations, we take the one-dimensional delta function δ h (x) to be the four-point delta function of Peskin [1]. The motion of the Lagrangian mesh nodes is determined in the cell-centered case via 10) and in the staggered-grid case via …”
Section: Eulerian and Lagrangian Spatial Discretizationsmentioning
confidence: 99%
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“…In our computations, we take the one-dimensional delta function δ h (x) to be the four-point delta function of Peskin [1]. The motion of the Lagrangian mesh nodes is determined in the cell-centered case via 10) and in the staggered-grid case via …”
Section: Eulerian and Lagrangian Spatial Discretizationsmentioning
confidence: 99%
“…To compute the m th component of N = (N 1 , N 2 ), we first determine a staggered-grid advection velocity field u ADV,m that is defined on the edges of the control volumes associated with component m of the velocity field u. Next, we use the xsPPM7 variant [10] of the piecewise-parabolic method (PPM) [11] to determine u PPM m , an upwind-biased interpolation of u m , on the edges of the control volumes, using u ADV,m to determine the upwind direction. Finally, for each component m of the velocity field, we evaluate N m = u ADV,m ·∇ h u PPM m using second-order compact finite differences.…”
Section: Approximating the Convective Acceleration Term U·∇umentioning
confidence: 99%
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“…Typically, these have been based on the idea allowing the representation of solution values outside the range defined by the cell averages [16], while still suppressing oscillations at discontinuities and underresolved gradients. In particular, the methods proposed to solve the problem to obtain uniform high-order accuracy for smooth solutions [6,8,7,13,2,10] typically have used quite elaborate analytic and / or geometric constructions. In this note, we propose a particularly simple approach to solving this problem for the PPM method [4].…”
Section: Introductionmentioning
confidence: 99%
“…We now turn to gas dynamics codes which have a broad range of applications, from astrophysical and geophysical flow simulation to the design and performance analysis of engineering systems. Specifically, we discuss the validation of the "Cuervo" code developed at Los Alamos National Laboratory [105,106] for use as a simulation tool in the complex physics of compressible mixing. This software generates solutions of the Euler equations for flows of inviscid, non-heat-conducting, compressible gas.…”
Section: A Computational Fluid Dynamics Model For Shock-induced Mixingmentioning
confidence: 99%