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Measurements were made in a large scale single stage turbine facility. Within the nozzle passage measurements were made using a five hole probe, a two-component Laser Doppler Velocimeter (LDV), and a single sensor hot wire probe. These measurements showed weak secondary flows at midchord, and two secondary flow loss cores at the nozzle exit. The casing vortex loss core was

Title : An Experimental Investigation of Steady and Unsteady Flow Field in an Axial Flow Turbine
Author : National Aeronautics and Space Administration
Language : en
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Type : PDF, ePub, Kindle
Uploaded : Apr 06, 2021

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