Three-dimensional steady supersonic duct flow using Lagrangian formulation-Reference-Cited by-同舟云学术

Three-dimensional steady supersonic duct flow using Lagrangian formulation

Published:1994-09 Issue:3 Volume:3 Page:239-248
ISSN:0938-1287
Container-title:Shock Waves
language:en
Short-container-title:Shock Waves

Author:

Loh C. Y.,Liou M. -S.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/BF01414718.pdf

Reference12 articles.

1. Anderson DA, Nangia RK (1977) Comparison of numerical and experimental ?conical? flow fields in supersonic corners with compression and/or expansion. Aeronautical Quarterly 28:293

2. Godunov SK (1959) A finite difference method for the numerical computation of discontinuous solutions of the equations of fluid dynamics. Matematicheskie Sbornik 47

3. Kutler P (1974) Supersonic flow in the corner formed by two intersecting wedges. AIAA Journal 12:577

4. Liou M-S (1987) A generalized procedure for constructing an upwind-based TVD scheme. AIAA paper 87-0355

5. Liou M-S, Hsu AT (1989) A time accurate finite volume high resolution scheme for three-dimensional Navier-Stokes equations. AIAA Paper 89-1994-CP

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