6th Conference of Iranian Aerospace Society , 2007-02-24

Title : ( ENO Scheme for Steady and Transient Compressible Flow in Pressure-Based Method )

Authors: Mohammad Hassan Djavareshkian , V. Enjilela ,

Citation: BibTeX | EndNote

Abstract

In this paper, a scheme based on Essentially Nonoscillating (ENO) has been developed into an implicit finite volume procedure, which uses pressure as a working variable. The boundedness criteria determined from ENO schemes. This numerical process is used for solution of Euler equations on a nonorthogonal mesh with collocated finite volume formulation. The developed scheme is applied to the computation of steady subsonic and transonic flows over a bump-in-channel geometry as well as to the transient shock-tube problem. The results of the ENO scheme are compared with analytical and other computations published in literature.

Keywords

, Finite Volume, ENO, Transient
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@inproceedings{paperid:1011759,
author = {Djavareshkian, Mohammad Hassan and V. Enjilela},
title = {ENO Scheme for Steady and Transient Compressible Flow in Pressure-Based Method},
booktitle = {6th Conference of Iranian Aerospace Society},
year = {2007},
location = {تهران, IRAN},
keywords = {Finite Volume; ENO; Transient},
}

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%0 Conference Proceedings
%T ENO Scheme for Steady and Transient Compressible Flow in Pressure-Based Method
%A Djavareshkian, Mohammad Hassan
%A V. Enjilela
%J 6th Conference of Iranian Aerospace Society
%D 2007

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