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Computational and Applied Mathematics Journal

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Comparison Among MUSCL, ENO and WENO Procedures as Applied to Reentry Flows in 2D

Computational and Applied Mathematics Journal
Vol.1 , No. 5, Publication Date: Jul. 13, 2015, Page: 355-377

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Authors

[1]	Edisson S. G. Maciel, Aeronautical Engineering Division (IEA), Aeronautical Technological Institute (ITA), SP, Brasil.

Abstract

In this work, a comparison among the second-order MUSCL procedure, the second-, third-, fourth- and fifth-order ENO procedure, and the third- and fifth-order WENO procedure is presented. The Euler and Navier-Stokes equations, on a finite volume and structured contexts, are studied. The numerical algorithm of Van Leer is used to perform the reentry flow numerical experiments. The “hot gas” hypersonic flow around a blunt body, in two-dimensions, is simulated. The results have indicated that the 4th and 5th order variants of the ENO procedure and the 3rd order variant of the WENO procedure have yielded the best solutions.

Keywords

MUSCL Procedure, ENO Procedure, WENO Procedure, Reentry Flows, Euler and Navier-Stokes Equations, Newton Interpolation Process, Finite Volume

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