Volume 22, Issue 1 (7-2003)                   JCME 2003, 22(1): 155-165 | Back to browse issues page

XML Persian Abstract Print

Download citation:
BibTeX | RIS | EndNote | Medlars | ProCite | Reference Manager | RefWorks
Send citation to:

H. Khaleghi, M. Mirzaee and S. M. H. Karimian. Development of an Upwind Algorithm at Subsonic Regions in the Solution of PNS Equations. JCME. 2003; 22 (1) :155-165
URL: http://jcme.iut.ac.ir/article-1-279-en.html
Abstract:   (2036 Views)
In this paper an upwind algorithm based on Roe’s scheme is presented for solution of PNS equations. Non iterative-implicit method using finite volume technique is used. The main advantage of this approach, in comparison with similar upwind methods, is reduction of oscillations around sonic line. This advantage causes the present method to be able to analyze supersonic flows with free stream Mach number near to one, where similar upwind methods normally fail. Some two dimensional/ axisymmetric test cases have been computed to validate the present method. These cases are: Hypersonic flow over a 15-degree compression ramp, two-dimensional supersonic flow over a flat plate and axisymmetric supersonic flow over a tangent ogive. The results are compared with the results of other numerical schemes, such as Beam and Warming scheme Keywords: Upwind, Navier stokes, Hypersonic
Full-Text [PDF 356 kb]   (485 Downloads)    
Type of Study: Research | Subject: General
Received: 2014/10/25 | Published: 2003/07/15

Add your comments about this article : Your username or Email:

© 2020 All Rights Reserved | Computational Methods in Engineering

Designed & Developed by : Yektaweb