scholarly journals On Low Mach Number Preconditioning of Finite Volume Schemes

PAMM ◽  
2005 ◽  
Vol 5 (1) ◽  
pp. 759-760 ◽  
Author(s):  
Philipp Birken ◽  
Andreas Meister
Author(s):  
Pascal Omnes ◽  
Stéphane Dellacherie ◽  
Jonathan Jung

Classical finite volume schemes for the Euler system  are not accurate at low Mach number and some fixes have to be used and were developed in a vast literature over the last two decades. The question we are interested in in this article is: What about if the porosity is no longer uniform? We first show that this problem may be understood on the linear wave equation taking into account porosity. We explain the influence of the cell geometry on the accuracy property at low Mach number. In the triangular case, the stationary space of the Godunov scheme approaches well enough the continuous space of constant pressure and divergence-free velocity, while this is not the case in the Cartesian case. On Cartesian meshes, a fix is proposed and accuracy at low Mach number is proved to be recovered. Based on the linear study, a numerical scheme and a low Mach fix for the non-linear system, with a non-conservative source term due to the porosity variations, is proposed and tested.


2018 ◽  
Vol 336 ◽  
pp. 368-393 ◽  
Author(s):  
Nicholas Simmonds ◽  
Panagiotis Tsoutsanis ◽  
Antonis F. Antoniadis ◽  
Karl W. Jenkins ◽  
Adrian Gaylard

2014 ◽  
Vol 271 ◽  
pp. 360-378 ◽  
Author(s):  
A. Bermúdez ◽  
J.L. Ferrín ◽  
L. Saavedra ◽  
M.E. Vázquez-Cendón

2011 ◽  
Vol 110-116 ◽  
pp. 423-430 ◽  
Author(s):  
Kazem Hejranfar ◽  
Ramin Kamali Moghadam

In the present study, two preconditioners proposed by Eriksson, and Choi and Merkel are implemented on a 3D upwind Euler flow solver on unstructured meshes. The mathematical formulations of these preconditioning schemes for the set of primitive variables are drawn and their eigenvalues and eigenvectors are compared with each others. A cell-centered finite volume Roe's method is used for discretization of the 3D preconditioned Euler equations. The accuracy and performance of these preconditioning schemes are examined by computing low Mach number flows over the ONERA M6 wing for different conditions.


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