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NASA NTRS ยท 20050217032

Courant Number and Mach Number Insensitive CE/SE Euler Solvers

Abstract

It has been known that the space-time CE/SE method can be used to obtain ID, 2D, and 3D steady and unsteady flow solutions with Mach numbers ranging from 0.0028 to 10. However, it is also known that a CE/SE solution may become overly dissipative when the Mach number is very small. As an initial attempt to remedy this weakness, new 1D Courant number and Mach number insensitive CE/SE Euler solvers are developed using several key concepts underlying the recent successful development of Courant number insensitive CE/SE schemes. Numerical results indicate that the new solvers are capable of resolving crisply a contact discontinuity embedded in a flow with the maximum Mach number = 0.01.

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BibTeXRIS

Chang, Sin-Chung. 2005-09-01. Courant Number and Mach Number Insensitive CE/SE Euler Solvers. https://ntrs.nasa.gov/citations/20050217032

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