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Quantification of Ice Accretions for Icing Scaling EvaluationsThe comparison of ice accretion characteristics is an integral part of aircraft icing research. It is often necessary to compare an ice accretion obtained from a flight test or numerical simulation to one produced in an icing wind tunnel or for validation of an icing scaling method. Traditionally, this has been accomplished by overlaying two-dimensional tracings of ice accretion shapes. This paper addresses the basic question of how to compare ice accretions using more quantitative methods. For simplicity, geometric characteristics of the ice accretions are used for the comparison. One method evaluated is a direct comparison of the percent differences of the geometric measurements. The second method inputs these measurements into a fuzzy inference system to obtain a single measure of the goodness of the comparison. The procedures are demonstrated by comparing ice shapes obtained in the Icing Research Tunnel at NASA Glenn Research Center during recent icing scaling tests. The results demonstrate that this type of analysis is useful in quantifying the similarity of ice accretion shapes and that the procedures should be further developed by expanding the analysis to additional icing data sets.
Document ID
20030068097
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Ruff, Gary A.
(NASA Glenn Research Center Cleveland, OH, United States)
Anderson, David N.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2003
Subject Category
Air Transportation And Safety
Report/Patent Number
NAS 1.15:212308
E-13891
NASA/TM-2003-212308
AIAA Paper 98-0195
Report Number: NAS 1.15:212308
Report Number: E-13891
Report Number: NASA/TM-2003-212308
Report Number: AIAA Paper 98-0195
Meeting Information
Meeting: 36th Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 12, 2003
End Date: January 15, 2003
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS-22-708-20-18
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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