INFLUENCE OF FLOW PARAMETERS AT THE BLADE CASCADE INLET UPON THE CHARACTERISTIC VALUES OF THE BOUNDARY LAYER ON THE TURBINE BLADE.

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作者
Pimsner, V.
Baran, N.
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FLOW OF FLUIDS - Boundary Layer - GAS TURBINES - Blades;
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摘要
The present paper sets out a calculation method meant to determine the boundary layer structure on the contour of the turbine blade profile, disposed within the cascade, under given flow conditions. It contains an analysis of the effects of the flow velocity value and cascade inlet angle upon the momentum deficit thickness of the boundary layer on the outer contour of the blade profile.
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页码:147 / 152
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