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contributor authorM. Nallasamy
contributor authorB. J. Clark
contributor authorJ. F. Groeneweg
date accessioned2017-05-08T23:26:00Z
date available2017-05-08T23:26:00Z
date copyrightJuly, 1987
date issued1987
identifier issn0889-504X
identifier otherJOTUEI-28585#332_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103209
description abstractThis paper presents the results of an investigation of the effects of far field boundary conditions on the solution of the three-dimensional Euler equations governing the flow field of a high-speed single rotation propeller. The results show that the solutions obtained with the nonreflecting boundary conditions are in good agreement with experimental data. The specification of nonreflecting boundary conditions is effective in reducing the dependence of the solution on the location of the far field boundary. Details of the flow field within the blade passage and the tip vortex are presented. The dependence of the computed power coefficient on the blade setting angle is examined.
publisherThe American Society of Mechanical Engineers (ASME)
titleEuler Analysis of the Three-Dimensional Flow Field of a High-Speed Propeller: Boundary Condition Effects
typeJournal Paper
journal volume109
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262110
journal fristpage332
journal lastpage339
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsBoundary-value problems
keywordsPropellers
keywordsBlades
keywordsRotation
keywordsWake turbulence AND Equations
treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 003
contenttypeFulltext


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