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contributor authorK. F. Weber
contributor authorD. W. Thoe
contributor authorR. A. Delaney
date accessioned2017-05-08T23:34:05Z
date available2017-05-08T23:34:05Z
date copyrightJuly, 1990
date issued1990
identifier issn0889-504X
identifier otherJOTUEI-28604#362_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107720
description abstractA three-dimensional Euler analysis for turbomachinery flows on a C-type grid is presented. The analysis is based on the Beam and Warming implicit algorithm for solution of the unsteady Euler equations and is derived from the ARC3D code developed by Pulliam at NASA Ames Research Center. Modifications made to convert this code from external flow applications to internal turbomachinery flows are given in detail. These changes include the addition of inflow, outflow, and periodic boundary point calculation procedures. Also presented are the C-grid construction procedures. Finally, results of code experimental verification studies for three-dimensional compressor cascade and rotor flows are presented.
publisherThe American Society of Mechanical Engineers (ASME)
titleAnalysis of Three-Dimensional Turbomachinery Flows on C-Type Grids Using an Implicit Euler Solver
typeJournal Paper
journal volume112
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927668
journal fristpage362
journal lastpage369
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsTurbomachinery
keywordsInflow
keywordsOutflow
keywordsCompressors
keywordsConstruction
keywordsCascades (Fluid dynamics)
keywordsAlgorithms
keywordsRotors AND Equations
treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 003
contenttypeFulltext


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