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contributor authorJ. Z. Xu
contributor authorW. Y. Ni
contributor authorJ. Y. Du
date accessioned2017-05-08T23:25:58Z
date available2017-05-08T23:25:58Z
date copyrightOctober, 1987
date issued1987
identifier issn0889-504X
identifier otherJOTUEI-28586#508_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103189
description abstractIn order to develop the transonic stream function approach, in this paper one of the momentum equations is employed to form the principal equation of the stream function which does not contain vorticity and entropy terms, and the other one is used to calculate the density directly. Since the density is uniquely determined, the problem that the density is a double-valued function of mass flux in the stream function formulation disappears and the entropy increase across the shock is naturally included. The numerical results for the transonic cascade flow show that the shock obtained from the present method is slightly weaker and is placed farther downstream compared to the irrotational stream function calculation, and is closer to the experimental data. From a standpoint of computation the iterative procedure of this formulation is simple and the alternating use of two momentum equations makes the calculation more effective.
publisherThe American Society of Mechanical Engineers (ASME)
titleNumerical Solution of Stream Function Equations in Transonic Flows
typeJournal Paper
journal volume109
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262140
journal fristpage508
journal lastpage512
identifier eissn1528-8900
treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 004
contenttypeFulltext


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