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High Order Resolution Applied to Chemical Non-Equilibrium Reentry Flows in 3D

Computational and Applied Mathematics Journal
Vol.1 , No. 5, Publication Date: Jul. 10, 2015, Page: 282-306

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Authors

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

Abstract

In this work, the ENO procedure is presented to a conserved variable interpolation process, using either the Newton method, to second-, third-, fourth- and fifth-orders of accuracy, or the Hermite method, to third- and fifth-orders of accuracy, and the WENO procedure is also presented to generate third- and fifth-orders of accuracy in the solution of the reactive Euler and Navier-stokes equations. The numerical algorithms of Van Leer and Liou and Steffen Jr. are employed. The “hot gas” hypersonic flow around a blunt body is simulated. The results have indicated that the ENO 4th order interpolation presents better solutions.

Keywords

Euler and Navier-Stokes Equations, MUSCL Procedure, ENO Procedure, WENO Procedure, Van Leer Algorithm, Liou and Steffen Jr. Algorithm, Three-Dimensions

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