Boundary Layer Development on a Turbine Blade in a Linear Cascade

20070038974 · NASA · 2007

Public domain · NASATechnical Reports

Overview

Several different boundary-layer development patterns for flow over the suction surface of a turbine airfoil in a linear cascade were studied and documented using a sliding surface hot-film sensor. The state of the boundary layer, whether laminar, transitional or turbulent, was determined at…

Publisher: NASA
Document: 20070038974
Year: 2007
Pages: 26

Document

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