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Title:Effects of Supercooled Large -Droplet Icing on Airfoil Aerodynamics
Author(s):Lee, Sam
Doctoral Committee Chair(s):Bragg, Michael B.
Department / Program:Aerospace Engineering
Discipline:Aerospace Engineering
Degree Granting Institution:University of Illinois at Urbana-Champaign
Degree:Ph.D.
Genre:Dissertation
Subject(s):Engineering, Aerospace
Abstract:The effects of simulated ice shape on the NLF 0414 were quite different from the NACA 23012m. There was little variation of lift when the simulated ice-shape location was varied from 2% to 20% chord. The large losses in lift occurred when the ice shape was located downstream of 30% chord, and the separation bubble formed over the adverse pressure gradient of the clean airfoil, which started at 75% chord. The effect of the ice shape on the NLF 0414 was not as severe as on the NACA 23012m because the lift was much more aft loaded.
Issue Date:2001
Type:Text
Language:English
Description:288 p.
Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2001.
URI:http://hdl.handle.net/2142/85067
Other Identifier(s):(MiAaPQ)AAI3017141
Date Available in IDEALS:2015-09-25
Date Deposited:2001


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