A finite difference scheme for steady, supersonic, two-dimensional, compressible flow of real gasesGlaister, P. (1992) A finite difference scheme for steady, supersonic, two-dimensional, compressible flow of real gases. Computers & Mathematics with Applications, 24 (4). pp. 49-59. ISSN 0898-1221 Full text not archived in this repository. It is advisable to refer to the publisher's version if you intend to cite from this work. See Guidance on citing. To link to this item DOI: 10.1016/0898-1221(92)90006-4 Abstract/SummaryA finite difference scheme is presented for the solution of the two-dimensional equations of steady, supersonic, compressible flow of real gases. The scheme incorparates numerical characteristic decomposition, is shock-capturing by design and incorporates space-marching as a result of the assumption that the flow is wholly supersonic in at least one space dimension. Results are shown for problems involving oblique hydraulic jumps and reflection from a wall.
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