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APPLICATION OF UNO SCHEME FOR STEADY AND TRANSIENT COMPRESSIBLE FLOW IN PRESSURE-BASED METHOD

نویسنده:
محمدحسن جوارشکیان
,
مصطفی فرنک
,
Mohammad Hassan Djavareshkian
سال
: 2008
چکیده: A pressure_based implicit procedure to solve the Euler equations on a nonorthogonal mesh with



collocated finite volume formulations is described which uses pressure as a working variable. The



boundedness criteria for this procedure are determined from Uniformly high_order accurate Non



Oscillatory (UNO) schemes, which are based on characteristic variables and are applied to the fluxes



of the convected quantities directly, including mass flow rate. The developed scheme is applied to



the computation of steady transonic and supersonic flow over a bump in channel geometry for



various Mach number as well as to the transient shock tube problem. Also the results of steady



supersonic flow over a ramp are presented. Then the results are compared with data predicted by



TVD schemes based on characteristic variables.
یو آر آی: http://libsearch.um.ac.ir:80/fum/handle/fum/3368309
کلیدواژه(گان): high resolution,Finite volume,UNO,TVD,transient,supersonic
کالکشن :
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    APPLICATION OF UNO SCHEME FOR STEADY AND TRANSIENT COMPRESSIBLE FLOW IN PRESSURE-BASED METHOD

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contributor authorمحمدحسن جوارشکیانen
contributor authorمصطفی فرنکen
contributor authorMohammad Hassan Djavareshkianfa
date accessioned2020-06-06T13:46:11Z
date available2020-06-06T13:46:11Z
date issued2008
identifier urihttp://libsearch.um.ac.ir:80/fum/handle/fum/3368309
description abstractA pressure_based implicit procedure to solve the Euler equations on a nonorthogonal mesh with



collocated finite volume formulations is described which uses pressure as a working variable. The



boundedness criteria for this procedure are determined from Uniformly high_order accurate Non



Oscillatory (UNO) schemes, which are based on characteristic variables and are applied to the fluxes



of the convected quantities directly, including mass flow rate. The developed scheme is applied to



the computation of steady transonic and supersonic flow over a bump in channel geometry for



various Mach number as well as to the transient shock tube problem. Also the results of steady



supersonic flow over a ramp are presented. Then the results are compared with data predicted by



TVD schemes based on characteristic variables.
en
languageEnglish
titleAPPLICATION OF UNO SCHEME FOR STEADY AND TRANSIENT COMPRESSIBLE FLOW IN PRESSURE-BASED METHODen
typeJournal Paper
contenttypeExternal Fulltext
subject keywordshigh resolutionen
subject keywordsFinite volumeen
subject keywordsUNOen
subject keywordsTVDen
subject keywordstransienten
subject keywordssupersonicen
journal titleJournal of applied sciencesen
journal titleJournal of Applied Sciencesfa
pages3361-3370
journal volume8
journal issue19
identifier linkhttps://profdoc.um.ac.ir/paper-abstract-1008306.html
identifier articleid1008306
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