25th AIAA Applied Aerodynamics Conference 2007
DOI: 10.2514/6.2007-4431
|View full text |Cite
|
Sign up to set email alerts
|

Implicit WENO Scheme and High Order Viscous Formulas for Compressible Flows

Abstract: The purpose of this paper is to develop a robust and efficient high order fully conservative finite difference scheme for compressible Navier-Stokes equations. The 5th order WENO scheme is used for the inviscid fluxes. A conservative fourth order accuracy finite central differencing scheme is developed for the viscous terms. An improved ε value of 10 −2 is suggested for the WENO smooth factors calculation, which removes the weight oscillation and significantly improves the convergence rate and level. The wall … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
60
0

Year Published

2010
2010
2017
2017

Publication Types

Select...
5
2
1

Relationship

1
7

Authors

Journals

citations
Cited by 60 publications
(60 citation statements)
references
References 19 publications
0
60
0
Order By: Relevance
“…∂F v ∂ξ can be discretized by a simple and straightforward central difference scheme while ∂F v ∂ξ must be treated more carefully to achieve grid level coupling and eliminate possible odd-even decoupling [25,31] problem. However, both of them can be written into conservative form.…”
Section: Governing Equations and Numerical Methodsmentioning
confidence: 99%
See 1 more Smart Citation
“…∂F v ∂ξ can be discretized by a simple and straightforward central difference scheme while ∂F v ∂ξ must be treated more carefully to achieve grid level coupling and eliminate possible odd-even decoupling [25,31] problem. However, both of them can be written into conservative form.…”
Section: Governing Equations and Numerical Methodsmentioning
confidence: 99%
“…The use of the Euler equations in primitive-variable form makes the formulas of the characteristic variables very simple. (2) A conservative, high order discretization for the viscous fluxes proposed in [25] is improved to make the computation more efficient, and the corresponding extrapolation procedures for computing the physical and numerical viscous fluxes at the boundary are also proposed. (3) The present boundary treatment procedure is designed for the curvilinear coordinates, which can be used together with finite difference schemes to solve problems on general geometries.…”
Section: Introductionmentioning
confidence: 99%
“…This term vanishes at the end of each physical time step, and has no influence on the accuracy of the solution. An implicit pseudo time marching scheme using Gauss-Seidel line relaxation is employed to achieve high convergence rate instead of using the explicit scheme [27]. The pseudo temporal term is discretized with first order Euler scheme.…”
Section: Time Marching Schemementioning
confidence: 99%
“…3 The nonlinear weight functionsw (r) j+1/2 , r = {L, C, R} used in equation (13), are constructed such that the interface fluxf j+ 1 2 is a convex combination of the three candidate second-order fluxes. The weight functions are constructed using the expressions…”
Section: General Structure Of Esweno Schemesmentioning
confidence: 99%