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University of Illinois at Urbana-Champaign
An Experimental Study of the Flowfield on a Semispan Rectangular Wing With a Simulated Glaze Ice Accretion
Abstract
dc:descriptionThe effect of a simulated glaze ice accretion on the flowfield of a semispan, reflection-plane, rectangular wing at Re = 1.5 million and M = 0.12 was investigated. A laser Doppler velocimeter was used to map the flowfield on the upper surface of the model in both the clean and iced configurations at α = 0, 4, and 8 degrees angle of attack.
Degree
thesis:*- Name thesis:degree_name
- Ph.D.
- Level thesis:degree_level
- Dissertation
- Discipline thesis:degree_discipline
- Aeronautical and Astronautical Engineering
- Grantor
- University of Illinois at Urbana-Champaign
- Year dc:date
- 2014
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Khodadoust, Abdollah
- Contributors dc:contributor
-
- Bragg, M.B.,
Subjects
dc:subject × 1Identifiers
dc:identifier.*- Identifier
- (UMI)AAI9314893
- OAI identifier oai:identifier
- oai:www.ideals.illinois.edu:2142/72368