Preconditioned methods for solving the incompressible low speed compressible equations
Journal of Computational Physics
Efficient implementation of essentially non-oscillatory shock-capturing schemes
Journal of Computational Physics
Advances in Applied Mathematics
The application of preconditioning in viscous flows
Journal of Computational Physics
A coupled implicit method for chemical non-equilibrium flows at all speeds
Journal of Computational Physics
Journal of Computational Physics
Efficient implementation of weighted ENO schemes
Journal of Computational Physics
Approximate Riemann solvers, parameter vectors, and difference schemes
Journal of Computational Physics - Special issue: commenoration of the 30th anniversary
A unified method for computing incompressible and compressible flows in boundary-fitted coordinates
Journal of Computational Physics
On the cancellation problem in calculating compressible low Mach number flows
Journal of Computational Physics
Asymptotic single and multiple scale expansions in the low Mach number limit
SIAM Journal on Applied Mathematics
On the use of higher-order finite-difference schemes on curvilinear and deforming meshes
Journal of Computational Physics
High-resolution viscous flow simulations at arbitrary Mach number
Journal of Computational Physics
Essentially Non-Oscillatory and Weighted Essentially Non-Oscillatory Schemes for Hyperbolic Conservation Laws
High order one-step monotonicity-preserving schemes for unsteady compressible flow calculations
Journal of Computational Physics
Handbook of Mathematical Functions, With Formulas, Graphs, and Mathematical Tables,
Handbook of Mathematical Functions, With Formulas, Graphs, and Mathematical Tables,
Journal of Computational Physics
Hi-index | 31.45 |
The inviscid low Mach number compressible flow developing from a plane incompressible vortex with constant density in a bounded domain is studied. A reference solution for this model flow is obtained by two-time scale asymptotic development in the zero Mach number limit. The solution can be decomposed into variations with a slow convective and a fast acoustic time scale. A selection of numerical schemes widely used to solve unsteady compressible low Mach number flows has been implemented to simulate this flow for two Mach number values, M=0.1 and M=0.01. The ability of the schemes to predict low Mach number flows and their behavior with the value of the Mach number have been analyzed.