Qin, N. (1992) A Comparative Study of Two Upwind Schemes as Applied to Navier-Stokes Solutions for Resolving Boundary Layers in Hypersonic Viscous Flow. G.U. Aero Report 9120. Technical Report. Department of Aerospace Engineering, University of Glasgow.
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Abstract
Van Leer's flux vector splitting scheme and Osher's flux difference splitting scheme are compared for solving the Navier-Stokes equations governing the hypersonic viscous flow. The effects of the grid number, the grid stretching, and the strength of the hmiter on the solution are studied for both of the schemes. Sensitivity of the results to these parameters are then compared for the two schemes.
| Item Type: | Research Reports or Papers (Technical Report) |
|---|---|
| Additional Information: | University of Glasgow author: N. Qin |
| Status: | Published |
| Glasgow Author(s) Enlighten ID: | UNSPECIFIED |
| Authors: | Qin, N. |
| College/School: | College of Science and Engineering > School of Engineering > Autonomous Systems and Connectivity |
| Publisher: | Department of Aerospace Engineering, University of Glasgow |
| Copyright Holders: | Copyright © 1992 Department of Aerospace Engineering, University of Glasgow |
| Publisher Policy: | Reproduced with the permission of the Department |
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