A non-uniform mesh scheme for compressible flow

Citations of this article
Mendeley users who have this article in their library.


A non-uniform mesh scheme is presented for the computation of compressible flows governed by the Euler equations of gas dynamics. The scheme is based on flux-difference splitting and represents an extension of a similar scheme designed for uniform meshes. The numerical results demonstrate that little, if any, spurious oscillation occurs as a result of the non-uniformity of the mesh; and importantly, shock speeds are computed correctly. © 1991.




Glaister, P. (1991). A non-uniform mesh scheme for compressible flow. Computers and Mathematics with Applications, 21(4), 39–62. https://doi.org/10.1016/0898-1221(91)90246-Z

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free