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Helium bubble flow visualization of the spanwise separation on a NACA 0012 with simulated glaze iceResearch has been performed to experimentally visualize and document the flow separation due to simulated glaze ice accretion on a NACA 0012 semispan with 30-deg sweep using helium bubbles as flow tracers. Results are compared to Navier-Stokes computational simulations for different angles of attack. Prior to acquiring data for the semispan model, a two-dimensional experiment was conducted to determine the accuracy of using the helium bubbles as flow tracers. Results from the 3D experiment compare well to the computational simulations.
Document ID
19920045568
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kerho, M.
(NASA Lewis Research Center Cleveland, OH, United States)
Bragg, M.
(Illinois, University Urbana, United States)
Shin, J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 92-0413
Accession Number
92A28192
Funding Number(s)
CONTRACT_GRANT: NAG3-1134
Distribution Limits
Public
Copyright
Other

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