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contributor authorM. Dittmann
contributor authorT. Geis
contributor authorV. Schramm
contributor authorS. Kim
contributor authorS. Wittig
date accessioned2017-05-09T00:09:03Z
date available2017-05-09T00:09:03Z
date copyrightJanuary, 2002
date issued2002
identifier issn0889-504X
identifier otherJOTUEI-28693#119_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/127665
description abstractThe discharge behavior of a “direct-transfer” preswirl system has been investigated experimentally. The influences of the pressure ratio and the swirl ratio as well as the influence of the receiver and stator geometry were investigated. The discharge coefficients of the preswirl nozzles are given in the absolute frame of reference. The definition of the discharge coefficient of the receiver holes is applied to the rotating system in order to consider the work done by the rotor. Numerical calculations carried out for a free expansion through the stationary preswirl nozzles show very good agreement with experimental data.
publisherThe American Society of Mechanical Engineers (ASME)
titleDischarge Coefficients of a Preswirl System in Secondary Air Systems
typeJournal Paper
journal volume124
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1413474
journal fristpage119
journal lastpage124
identifier eissn1528-8900
keywordsNozzles
keywordsRotors
keywordsDischarge coefficient
keywordsPressure
keywordsFlow (Dynamics)
keywordsStators
keywordsStructural frames AND Temperature
treeJournal of Turbomachinery:;2002:;volume( 124 ):;issue: 001
contenttypeFulltext


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