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Published in:
2018 | OriginalPaper | Chapter
Incidence and Deviation
Author : Meinhard T. Schobeiri
Published in: Gas Turbine Design, Components and System Design Integration
Publisher: Springer International Publishing
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Up to this point, the relationships developed for a turbomachinery stage have been strictly correct for given velocity diagrams with known inlet and exit flow angles. We assumed that the flow is fully congruent with the blade profile. This assumption implies that the inlet and exit flow angles coincide with the camber angles at the leading and trailing edges.