Assessment of SLAU2 and other flux functions with slope limiters in hypersonic shock-interaction heating
From MaRDI portal
Publication:1646864
DOI10.1016/j.compfluid.2016.02.006zbMath1390.76281OpenAlexW2284281614MaRDI QIDQ1646864
Publication date: 26 June 2018
Published in: Computers and Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.compfluid.2016.02.006
Related Items
An effective flux scheme for hypersonic heating prediction of re-entry vehicles ⋮ SLAU2 applied to two-dimensional, ideal magnetohydrodynamics simulations ⋮ Immersed boundary conditions for hypersonic flows using ENO-like least-square reconstruction
Uses Software
Cites Work
- Towards shock-stable and accurate hypersonic heating computations: a new pressure flux for AUSM-family schemes
- High resolution schemes for hyperbolic conservation laws
- Approximate Riemann solvers, parameter vectors, and difference schemes
- Restoration of the contact surface in the HLL-Riemann solver
- Modified SLAU2 scheme with enhanced shock stability
- Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method
- Robust HLL-type Riemann solver capable of resolving contact discontinuity
- Very simple, carbuncle-free, boundary-layer-resolving, rotated-hybrid Riemann solvers
- A sequel to AUSM II: AUSM\(^+\)-up for all speeds
- On Upstream Differencing and Godunov-Type Schemes for Hyperbolic Conservation Laws
- On Godunov-Type Methods for Gas Dynamics
- A point implicit unstructured grid solver for the euler and Navier-Stokes equations
- Numerical solutions of Euler equations by using a new flux vector splitting scheme
- Application of essentially nonoscillatory schemes to unsteady hypersonic shock-shock interference heating problems
- Shock wave numerical structure and the carbuncle phenomenon
- Extension and Comparative Study of AUSM-Family Schemes for Compressible Multiphase Flow Simulations
- Numerical instabilities in upwind methods: Analysis and cures for the ``carbuncle phenomenon
- Methods for the accurate computations of hypersonic flows. I: AUSMPW+scheme
- Unnamed Item
- Unnamed Item
- Unnamed Item
