NASA NTRS · 19860063491
Three-dimensional fluid flow phenomena in the blade end wall corner region
Abstract
Flow visualization, static and total pressure measurements, and mean velocity profile measurements with a single-sensor inclined hot wire probe, are used in a study of three-dimensional flow at a turbine blade end wall corner region for six critical axial stations along the blade chord. Three vortices are identified: (1) a horseshoe vortex near the leading edge; (2) a corner eddy between the horseshoe vortex and the corner; and (3) a vortex at the rear portion of the corner due to the corner eddy's secondary flow. Attention is given to the relative size and rate-of-spread of the vortices in the streamwise direction.
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Hazarika, B. K., Raj, R., Boldman, D. R.. 1986-06-01. Three-dimensional fluid flow phenomena in the blade end wall corner region. https://ntrs.nasa.gov/citations/19860063491
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