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A Study of the Effects of Altitude on Thermal Ice Protection System PerformanceThermal ice protection systems use heat energy to prevent a dangerous buildup of ice on an aircraft. As aircraft become more efficient, less heat energy is available to operate a thermal ice protections system. This requires that thermal ice protection systems be designed to more exacting standards so as to more efficiently prevent a dangerous ice buildup without adversely affecting aircraft safety. While the effects of altitude have always beeing taked into account in the design of thermal ice protection systems, a better understanding of these effects is needed so as to enable more exact design, testing, and evaluation of these systems.
Document ID
20140011436
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Addy, Gene
(NASA Glenn Research Center Cleveland, OH United States)
Oleskiw, Myron
(National Research Council of Canada Boucherville, Quebec, Canada)
Broeren, Andy P.
(NASA Glenn Research Center Cleveland, OH United States)
Orchard, David
(National Research Council of Canada Boucherville, Quebec, Canada)
Date Acquired
September 8, 2014
Publication Date
September 1, 2013
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
GRC-E-DAA-TN8913
AIAA Paper-2013-2934
E-18690-1
NASA/TM-2013-216559
Funding Number(s)
WBS: WBS 648987.02.03.03.10
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
thermal ice protection system
icing
icing scaling
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