Aircraft icing

This paper reviews the background to and the current status of analyses developed to address the problem of icing on aircraft. Methods for water droplet trajectory calculation, ice accretion prediction, aerodynamic performance degradation and an overview of ice protection system modelling are presen...

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Bibliographic Details
Published in:Philosophical transactions of the Royal Society of London. Series A: Mathematical, physical, and engineering sciences Vol. 358; no. 1776; pp. 2873 - 2911
Main Authors: Poots, G., Gent, R. W., Dart, N. P., Cansdale, J. T.
Format: Journal Article
Language:English
Published: The Royal Society 15-11-2000
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Summary:This paper reviews the background to and the current status of analyses developed to address the problem of icing on aircraft. Methods for water droplet trajectory calculation, ice accretion prediction, aerodynamic performance degradation and an overview of ice protection system modelling are presented. The paper addresses the issues involved in the development of icing analyses including problem formulation and assumptions, solution techniques, validation and the incorporation of empirical inputs where a purely theoretical approach is not feasible. Results are presented to illustrate the capabilities of the analyses when applied to practical design problems. Recommendations are made for further research.
Bibliography:istex:524F49E6AC8C32703A0AC6DA88F6E4A421B2B138
ark:/67375/V84-MN95L539-Z
Theme Issue 'Ice and snow accretion on structures' compiled by G. Poots
ObjectType-Article-1
SourceType-Scholarly Journals-1
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content type line 23
ISSN:1364-503X
1471-2962
DOI:10.1098/rsta.2000.0689