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Development of an automated non-axisymmetric endwall contour design system for the rotor of a 1-stage research turbine - Part 1 System Design

Author: Bergh, J ; Snedden, Glen C ; Reddy, D Date: Sep 2019 Secondary flows are a well-known source of loss in turbomachinery flows, contributing up to 30% of the total aerodynamic blade row loss. With the increase in pressure on aero-engine manufacturers to produce lighter, more powerful and increasingly ... Read more

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Browsing by Subject "DACE"

Browsing by Subject "DACE"

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