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contributor authorHans-Heiner Fruehauf
date accessioned2017-05-08T23:02:51Z
date available2017-05-08T23:02:51Z
date copyrightJanuary, 1977
date issued1977
identifier issn1528-8919
identifier otherJETPEZ-26730#115_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/89853
description abstractSolutions of the differential equations of the axisymmetric model and circumferentially averaged solutions of the differential equations of the three-dimensional model are compared quantitatively for steady supersonic flows through rotating annular cascades. Thereby three-dimensional corrections for flow quantities, which determine the applicability of the axisymmetric analysis, are investigated as a function of geometrical and gas dynamical parameters. Finally, these three-dimensional corrections are compared to three-dimensional corrections for the solutions of the usual blade-to-blade model on cylindrical surfaces of revolution for identical annular cascades.
publisherThe American Society of Mechanical Engineers (ASME)
titleApplicability of Axisymmetric Analysis in Predicting Supersonic Flow Through Annular Cascades
typeJournal Paper
journal volume99
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3446239
journal fristpage115
journal lastpage120
identifier eissn0742-4795
keywordsSupersonic flow
keywordsDifferential equations
keywordsBlades
keywordsThree-dimensional models AND Flow (Dynamics)
treeJournal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 001
contenttypeFulltext


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