Existing approximate Riemann solvers do not perform well when the grid is not aligned with strong shocks in the flow field. Three new approximate Riemann algorithms are investigated to improve solution accuracy and stability in the vicinity of strong shocks. The new algorithms are compared to the existing upwind algorithms in OVERFLOW 2.1. The new algorithms use a multidimensional pressure gradient based switch to transition to a more numerically dissipative algorithm in the vicinity of strong shocks. One new algorithm also attempts to artificially thicken captured shocks in order to alleviate the errors in the solution introduced by “stair-stepping ” of the shock resulting from the approximate Riemann solver. This algorithm performed well ...
From the early stages of CFD, the computation of shocks using Finite Volume methods has been a very ...
We describe an approximate Riemann solver for the computation of hypervelocity flows in which there ...
The numerical error produced when computing slowly moving shocks in a finite volume framework is stu...
We describe an approximate Riemann solver for the computation of hypervelocity flows in which there ...
A shock capturing scheme is presented for the equations of isentropic flow based on upwind differenc...
Within a continuum framework, flows featuring shock waves can be modelled by means of either shock c...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
Three topics on modern shock capturing methods for the time-dependent Euler equations of Gas Dynamic...
High-order methods that can resolve interactions of flow-disturbances with shock waves are critical ...
The accuracy of two grid adaptation strategies, grid redistribution and local grid refinement, is ex...
AbstractOur contribution reviews High Resolution Shock Capturing methods (HRSC) in the field of rela...
This thesis aims to assist the development of a multiblock implicit Navier-Stokes code for hyperson...
Summarization: This paper constructs, presents and compares four approximate Riemann solvers for use...
International audienceThe appearance of shock anomaly is a major unsolved problem for some low diffu...
In order to eliminate or minimize the numerical error by shock waves due to grid distribution in mul...
From the early stages of CFD, the computation of shocks using Finite Volume methods has been a very ...
We describe an approximate Riemann solver for the computation of hypervelocity flows in which there ...
The numerical error produced when computing slowly moving shocks in a finite volume framework is stu...
We describe an approximate Riemann solver for the computation of hypervelocity flows in which there ...
A shock capturing scheme is presented for the equations of isentropic flow based on upwind differenc...
Within a continuum framework, flows featuring shock waves can be modelled by means of either shock c...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
Three topics on modern shock capturing methods for the time-dependent Euler equations of Gas Dynamic...
High-order methods that can resolve interactions of flow-disturbances with shock waves are critical ...
The accuracy of two grid adaptation strategies, grid redistribution and local grid refinement, is ex...
AbstractOur contribution reviews High Resolution Shock Capturing methods (HRSC) in the field of rela...
This thesis aims to assist the development of a multiblock implicit Navier-Stokes code for hyperson...
Summarization: This paper constructs, presents and compares four approximate Riemann solvers for use...
International audienceThe appearance of shock anomaly is a major unsolved problem for some low diffu...
In order to eliminate or minimize the numerical error by shock waves due to grid distribution in mul...
From the early stages of CFD, the computation of shocks using Finite Volume methods has been a very ...
We describe an approximate Riemann solver for the computation of hypervelocity flows in which there ...
The numerical error produced when computing slowly moving shocks in a finite volume framework is stu...