Accessibility navigation


A finite difference scheme for steady, supersonic, two-dimensional, compressible flow of real gases

Glaister, 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/Summary

A 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.

Item Type:Article
Refereed:Yes
Divisions:Faculty of Science > School of Mathematical, Physical and Computational Sciences > Department of Mathematics and Statistics
ID Code:15645
Publisher:Elsevier

University Staff: Request a correction | Centaur Editors: Update this record

Page navigation