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Flow visualization study of the horseshoe vortex in a turbine stator cascadeFlow visualization techniques were used to show the behavior of the horseshoe vortex in a large scale turbine stator cascade. Oil drops on the end wall surface flowed in response to local shear stresses, indicating the limiting flow streamlines at the surface. Smoke injected into the flow and photographed showed time averaged flow behavior. Neutrally bouyant helium filled soap bubbles followed the flow and showed up on photographs as streaks, indicating the paths followed by individual fluid particles. Preliminary attempts to control the vortex were made by injecting air through control jets drilled in the end wall near the vane leading edge. Seventeen different hole locations were tested, one at a time, and the effect of the control jets on the path follwed by smoke in the boundary layer was recorded photographically.
Document ID
19820022622
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Gaugler, R. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Russell, L. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.60:1884
E-915
NASA-TP-1884
Report Number: NAS 1.60:1884
Report Number: E-915
Report Number: NASA-TP-1884
Accession Number
82N30498
Funding Number(s)
PROJECT: RTOP 505-32-2B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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