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contributor authorA. B. Wassell
date accessioned2017-05-09T00:06:16Z
date available2017-05-09T00:06:16Z
date copyrightApril, 1968
date issued1968
identifier issn1528-8919
identifier otherJETPEZ-26668#149_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126034
description abstractThe influence of variations in flow Reynolds number on the performance of axial compressors has been studied (changes in Reynolds number being, for the most part, achieved by changes in the inlet total pressure at or near the design speed). The measured results, so achieved, have been correlated to show how the main compressor performance parameters vary with Reynolds number. Reference has been made to cascade data to assist in choosing the form of the correlation, which is essentially empirical. A good correlation of the measured performance changes on component tests has been obtained. The method described, therefore, appears to be satisfactory for predicting trends for project assessments and avoids considering the detailed flow changes that occur within the machine as the Reynolds number is varied.
publisherThe American Society of Mechanical Engineers (ASME)
titleReynolds Number Effects in Axial Compressors
typeJournal Paper
journal volume90
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3609154
journal fristpage149
journal lastpage156
identifier eissn0742-4795
keywordsCompressors
keywordsReynolds number
keywordsFlow (Dynamics)
keywordsMachinery
keywordsPressure
keywordsCascades (Fluid dynamics) AND Design
treeJournal of Engineering for Gas Turbines and Power:;1968:;volume( 090 ):;issue: 002
contenttypeFulltext


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