Open AccessStreakline Flow Visualization Study of a Horseshoe Vortex in a Large-Scale, Two-Dimensional Turbine Stator Cascade
Author(s) -
Raymond E. Gaugler,
L. M. Russell
Publication year - 1980
Publication title -
nasa sti repository (national aeronautics and space administration)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.1115/80-gt-4
Subject(s) - streamlines, streaklines, and pathlines , vortex , flow visualization , mechanics , horseshoe vortex , reynolds number , chord (peer to peer) , leading edge , boundary layer , turbine , cascade , flow (mathematics) , physics , stator , materials science , vortex ring , turbulence , engineering , computer science , thermodynamics , distributed computing , quantum mechanics , chemical engineering
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.Copyright © 1980 by ASME
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