Previous studies of interface conditions satisfying one or more of the above criteria for various applications have concen-Multidomain treatments are studied in order to solve the steady compressible Euler equations using implicit time-dependent finite trated mainly on explicit difference schemes. C
Correction of Conservative Euler Solvers for Gas Mixtures
✍ Scribed by P. Jenny; B. Müller; H. Thomann
- Publisher
- Elsevier Science
- Year
- 1997
- Tongue
- English
- Weight
- 759 KB
- Volume
- 132
- Category
- Article
- ISSN
- 0021-9991
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✦ Synopsis
errors up to the truncation error. That second-order nonconservative scheme was employed by Quirk and Karni Conservative Euler solvers for gas mixtures produce numerical errors near contact discontinuities, if the temperature and the ratio [13] to simulate the interactions of plane shock waves with of specific heats are not constant there. For mixtures of perfect cylindrical gas bubbles contained in air using adaptive mesh gases, a simple correction of the total energy per unit volume is refinement. In another approach, Karni [8] solved the conproposed to avoid these errors. This is done in a physical way and servation laws augmented by the non-conservative energy only the total energy looses some of its conservativity. Numerical equation, identified the vicinity of the contact discontinusimulations of contact discontinuity convection, a shock tube problem, and shock-interface interactions in 1D and 2D yield much more ity, and switched there from a conservative formulation to accurate solutions, if the correction is applied. The straightforward a non-conservative one with regard to the energy equation.
Toro [17] used a non-conservative scheme, except for the vicinity of shock waves where the discretization is switched to a conservative scheme. However, since most flow solvers
📜 SIMILAR VOLUMES
In a recent paper [P. Glaister, Conservative upwind difference schemes for compressible flows in a Duct, Comput. Math. Appl. 56 (2008) 1787-1796] numerical schemes based on a conservative linearisation are presented for the Euler equations governing compressible flows of an ideal gas in a duct of va