Investigation for Loss Generation Mechanisms of Flow in Turbomachinery by Using Curved Square Duct

Autor:	Atsumasa Yamamoto, Shimpei Mizuki, Hoshio Tsujita
Rok vydání:	2006
Předmět:	Fluid Flow and Transfer Processes Pressure drop Physics business.industry Mechanical Engineering Mechanics Aerodynamics Secondary flow Boundary layer thickness Vortex Physics::Fluid Dynamics Axial compressor Optics Turbomachinery Duct (flow) Physical and Theoretical Chemistry business
Zdroj:	JSME International Journal Series B. 49:686-694
ISSN:	1347-5371 1340-8054
DOI:	10.1299/jsmeb.49.686
Popis:	In a series of present studies, the flows within the stationary curved ducts are analyzed numerically with the aerodynamic or the geometrical parameters affecting the loss generation caused by the passage vortex within a passage of a turbomachinery. In the former reports, the inlet boundary layer thickness and the inlet velocity distortion were taken as the aerodynamic parameter and the aspect ratio of the cross-section was chosen as the geometrical parameter. In this report, the effects of the curved angle of the bend on the loss generation caused by the passage vortex are examined by relating the bend of curved duct to the blade-to-blade surface of an axial flow turbine cascade. The curved angle is changed from 90 to 160 degrees by 10 degrees with fixing the length of arc for the mean radius of curvature of the bend or with fixing the mean radius of curvature.
Databáze:	OpenAIRE
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