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contributor authorH. S. Pordal
contributor authorP. K. Khosla
contributor authorS. G. Rubin
date accessioned2017-05-08T23:38:49Z
date available2017-05-08T23:38:49Z
date copyrightJune, 1992
date issued1992
identifier issn0098-2202
identifier otherJFEGA4-27067#198_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110448
description abstractThe solution of the reduced Navier Stokes (RNS) equations is considered using a flux-split procedure. Unsteady flow in a two dimensional engine inlet is computed. The problems of unstart and restart are investigated. A sparse matrix direct solver combined with a domain decomposition strategy is used to compute the unsteady flow field. Strong shock-boundary layer interaction, time varying shocks, and time varying recirculation regions are efficiently captured.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Flux-Split Solution Procedure for Unsteady Inlet Flow Calculations
typeJournal Paper
journal volume114
journal issue2
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.2910016
journal fristpage198
journal lastpage204
identifier eissn1528-901X
keywordsFlow (Dynamics)
keywordsEngines
keywordsShock (Mechanics)
keywordsEquations AND Unsteady flow
treeJournal of Fluids Engineering:;1992:;volume( 114 ):;issue: 002
contenttypeFulltext


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