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Problems in understanding aircraft icing dynamicsA general discussion of the nonthermodynamic mechanisms present during ice accretion on nonrotatig and rotating/flexing aerodynamic surfaces is undertaken. It is shown that competing physical effects do not in general allow a rigorous scaling methodology to be formulated, but suggestions are made which may result in an acceptable approxiamte scaling scheme. A test program is described which may provide data from which these approximate scaling schemes may be validated.
Document ID
19890038182
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bilanin, Alan J.
(Continuum Dynamics, Inc. Princeton, NJ, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Air Transportation And Safety
Report/Patent Number
AIAA PAPER 89-0735
Report Number: AIAA PAPER 89-0735
Accession Number
89A25553
Distribution Limits
Public
Copyright
Other

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