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Proposed modifications to ice accretion/icing scaling theoryThe difficulty of conducting full-scale icing tests has long been appreciated. Testing in an icing wind tunnel has been undertaken for decades. While aircraft size and speeds have increased, tunnel facilities have not, thus making subscale geometric tests a necessity. Scaling laws governing these tests are almost exclusively based on analysis performed over 30 years ago and have not been rigorously validated. The following work reviews past scaling analyses and suggests revision to these analyses based on recent experimental observation. It is also suggested, based on the analysis contained herein, that current ice accretion predictive technologies, such as LEWICE when utilized in the glaze ice accretion regime, may need upgrading to more accurately estimate the rate of ice build-up on aerodynamic surfaces.
Document ID
19880034923
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bilanin, Alan J.
(Continuum Dynamics, Inc. Princeton, NJ, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Air Transportation And Safety
Report/Patent Number
AIAA PAPER 88-0203
Accession Number
88A22150
Funding Number(s)
CONTRACT_GRANT: NAS1-18302
Distribution Limits
Public
Copyright
Other

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