Neutrally 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. Inlet Reynolds number, based on true chord, ranged between 1.0 × 10 ⅝ to 3.0 × 10 ⅝. 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.
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ASME 1980 International Gas Turbine Conference and Products Show
March 10–13, 1980
New Orleans, Louisiana, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7965-8
PROCEEDINGS PAPER
Streakline Flow Visualization Study of a Horseshoe Vortex in a Large-Scale, Two-Dimensional Turbine Stator Cascade
R. E. Gaugler,
R. E. Gaugler
National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH
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L. M. Russell
L. M. Russell
National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH
Search for other works by this author on:
R. E. Gaugler
National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH
L. M. Russell
National Aeronautics and Space Administration, Lewis Research Center, Cleveland, OH
Paper No:
80-GT-4, V01AT01A004; 8 pages
Published Online:
April 17, 2015
Citation
Gaugler, RE, & Russell, LM. "Streakline Flow Visualization Study of a Horseshoe Vortex in a Large-Scale, Two-Dimensional Turbine Stator Cascade." Proceedings of the ASME 1980 International Gas Turbine Conference and Products Show. Volume 1A: General. New Orleans, Louisiana, USA. March 10–13, 1980. V01AT01A004. ASME. https://doi.org/10.1115/80-GT-4
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