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NASA's Aircraft Icing Analysis ProgramAn overview of the NASA ongoing efforts to develop an aircraft icing analysis capability is presented. Discussions are included of the overall and long term objectives of the program as well as current capabilities and limitations of the various computer codes being developed. Descriptions are given of codes being developed to analyze two and three dimensional trajectories of water droplets, airfoil ice accretion, aerodynamic performance degradation of components and complete aircraft configurations, electrothermal deicer, fluid freezing point depressant antideicer and electro-impulse deicer. The need for bench mark and verification data to support the code development is also discussed, and selected results of experimental programs are presented.
Document ID
19860022076
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shaw, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Air Transportation And Safety
Report/Patent Number
E-3121
NASA-TM-88791
NAS 1.15:88791
Accession Number
86N31548
Funding Number(s)
PROJECT: RTOP 505-68-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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