Analysis and Improvement of Upwind and Centered Schemes on Quadrilateral and Triangular Meshes

Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781726207195


Pages:   42
Publication Date:   27 August 2018
Format:   Paperback
Availability:   Available To Order   Availability explained
We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately.

Our Price $65.97 Quantity:  
Add to Cart

Share |

Analysis and Improvement of Upwind and Centered Schemes on Quadrilateral and Triangular Meshes


Overview

Second-order accurate upwind and centered schemes are presented in a framework that facilitates their analysis and comparison. The upwind scheme employed consists of a reconstruction step (MUSCL approach) followed by an upwind step (Roe's flux-difference splitting). The two centered schemes are of Lax-Friedrichs (L-F) type. They are the nonstaggered versions of the Nessyahu-Tadmor (N-T) scheme and the CE/SE method with epilson = 1/2. The upwind scheme is extended to the case of two spatial dimensions (2D) in a straightforward manner. The N-T and CE/SE schemes are extended in a manner similar to the 2D extensions of the CE/SE scheme by Wang and Chang for a triangular mesh and by Zhang, Yu, and Chang for a quadrilateral mesh. The slope estimates, however, are simplified. Fourier stability and accuracy analyses are carried out for these schemes for the standard 1D and the 2D quadrilateral mesh cases. In the nonstandard case of a triangular mesh, the triangles must be paired up when analyzing the upwind and N-T schemes. An observation resulting in an extended N-T scheme which is faster and uses only one-third of the storage for flow data compared with the CE/SE method is presented. Numerical results are shown. Other improvements to the schemes are discussed.Huynh, H. T.Glenn Research CenterUPWIND SCHEMES (MATHEMATICS); COMPUTATIONAL FLUID DYNAMICS; FINITE DIFFERENCE THEORY; EULER EQUATIONS OF MOTION; STRUCTURED GRIDS (MATHEMATICS); SPACE-TIME CE/SE METHOD; FLOW EQUATIONS; TWO DIMENSIONAL MODELS; GRID GENERATION (MATHEMATICS); FOURIER ANALYSIS...

Full Product Details

Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
Imprint:   Createspace Independent Publishing Platform
Dimensions:   Width: 21.60cm , Height: 0.20cm , Length: 27.90cm
Weight:   0.122kg
ISBN:  

9781726207195


ISBN 10:   1726207196
Pages:   42
Publication Date:   27 August 2018
Audience:   General/trade ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   Available To Order   Availability explained
We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately.

Table of Contents

Reviews

Author Information

Tab Content 6

Author Website:  

Countries Available

All regions
Latest Reading Guide

April RG 26_2

 

Shopping Cart
Your cart is empty
Shopping cart
Mailing List