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contributor authorG. V. Hobson
contributor authorB. Lakshminarayana
date accessioned2017-05-08T23:36:53Z
date available2017-05-08T23:36:53Z
date copyrightOctober, 1991
date issued1991
identifier issn0889-504X
identifier otherJOTUEI-28615#561_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109349
description abstractA fully elliptic, control volume solution of the two-dimensional incompressible Navier–Stokes equations for the prediction of cascade performance over a wide range is presented in this paper. The numerical technique is based on a new pressure substitution method. A Poisson equation is derived from the pressure-weighted substitution of the full momentum equations into the continuity equation. The analysis of a double circular arc compressor cascade is presented, and the results are compared with the available experimental data at various incidence angles. Good agreement is obtained for the blade pressure distribution, boundary layer and wake profiles, skin friction coefficient, losses and outlet angles. Turbulence effects are simulated by the low-Reynolds-number version of the k–ε turbulence model.
publisherThe American Society of Mechanical Engineers (ASME)
titlePrediction of Cascade Performance Using an Incompressible Navier–Stokes Technique
typeJournal Paper
journal volume113
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2929115
journal fristpage561
journal lastpage571
identifier eissn1528-8900
keywordsCascades (Fluid dynamics)
keywordsPressure
keywordsTurbulence
keywordsEquations
keywordsPoisson equation
keywordsCompressors
keywordsMomentum
keywordsSkin friction (Fluid dynamics)
keywordsWakes
keywordsNavier-Stokes equations
keywordsBoundary layers AND Blades
treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 004
contenttypeFulltext


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