Numerical Investigation of Influence of Tangent Pitch and Slanting Flow of Guide Vanes on the Axial Compressor Stage Parameters

Numerical Investigation of Influence of Tangent Pitch and Slanting Flow of Guide Vanes on the Axial Compressor Stage Parameters

<p>The flow redistribution in the axial stage through the stator axis blade deformation can create favorable conditions for raising stage efficiency and combined actions for axial compressor elements especially in ambient conditions. For this purpose, the axis deformation impact on the gas-dyn...

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Bibliographic Details
Main Authors: D. V. Arkhipov, R. Z. Tumashev
Format: Article
Language:Russian
Published: MGTU im. N.È. Baumana 2015-01-01
Series:Nauka i Obrazovanie
Subjects:
axial compressor
stage
guide vane
numerical simulation
gas-dynamic stability margin
efficiency
tangent pitch
slanting flow
Online Access:http://technomag.edu.ru/jour/article/view/113

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