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Streakline flow visualization study of a horseshoe vortex in a large-scale, two-dimensional turbine stator cascadeNeutrally buoyant helium-filled bubbles were observed as they followed the streamlines in a horseshoe vortex system around the vane leading edge in a large-scale, two-dimensional, turbine stator cascade. Bubbles were introduced into the endwall boundary layer through a slot upstream of the vane leading edge. The paths of the bubbles were recorded photographically as streaklines on 16-mm movie film. Individual frames from the film have been selected, and overlayed to show the details of the horseshoe vortex around the leading edge. The transport of the vortex across the passage near the leading edge is clearly seen when compared to the streaks formed by bubbles carried in the main stream. Limiting streamlines on the endwall surface were traced by the flow of oil drops.
Document ID
19800057975
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gaugler, R. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Russell, L. M.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
ASME PAPER 80-GT-4
Meeting Information
Meeting: Gas Turbine Conference and Products Show
Location: New Orleans, LA
Start Date: March 10, 1980
End Date: March 13, 1980
Sponsors: American Society of Mechanical Engineers
Accession Number
80A42145
Distribution Limits
Public
Copyright
Other

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