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Surface roughness due to residual ice in the use of low power deicing systemsThicknesses of residual ice are presented to provide information on surface contamination and associated roughness during deicing events. Data was obtained from low power ice protection systems tests conducted in the Icing Research Tunnel at NASA Lewis Research Center (LeRC) with nine different deicing systems. Results show that roughness associated with residual ice is not characterized by uniformly distributed roughness. Results also show that deicing systems require a critical mass of ice to generate a sufficient expelling force to remove the ice.
Document ID
19930039243
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shin, Jaiwon
(NASA Lewis Research Center Cleveland, OH, United States)
Bond, Thomas H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-0031
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A23240
Funding Number(s)
PROJECT: RTOP 505-68-10
Distribution Limits
Public
Copyright
Other

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