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contributor authorN. Kyrtatos
contributor authorN. Watson
date accessioned2017-05-08T23:08:34Z
date available2017-05-08T23:08:34Z
date copyrightOctober, 1980
date issued1980
identifier issn1528-8919
identifier otherJETPEZ-26762#943_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93198
description abstractA design procedure is described which allows the development of an arrangement to aerodynamically impart prewhirl to the inflow of a compressor. The procedure uses compressor performance data and inducer inlet flow distributions together with a mathematical model of the aerodynamic prewhirl inducing arrangement to arrive at the parameters which completely define an arrangement suitable for a particular compressor. The application of the procedure to design an arrangement for a small turbocharger compressor is presented. The effect of the aerodynamically imparted prerotation on the compressor performance was found to be similar to that produced by inlet guide vanes.
publisherThe American Society of Mechanical Engineers (ASME)
titleApplication of Aerodynamically Induced Prewhirl to a Small Turbocharger Compressor
typeJournal Paper
journal volume102
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3230365
journal fristpage943
journal lastpage950
identifier eissn0742-4795
keywordsCompressors
keywordsDesign
keywordsInflow AND Flow (Dynamics)
treeJournal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 004
contenttypeFulltext


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