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Evaluation of Small Scale Icing Tunnel Test Results
Technical Paper
2007-01-3328
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
A test has been performed using a scaled aircraft wing section in an icing tunnel facility. The model had an electro-thermal ice protection system installed. The tests performed considered both anti-icing and de-icing modes of operation. The results have been assessed using numerical codes and the effect of model scaling has been considered. The non-scaled skin thickness of the model was found to modify the predicted behaviour of a full-scale installation, predominantly due to lateral conduction effects. The extent of this has been assessed and recommendations are made as to the performance that may be expected at full-scale.
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Citation
Barley, S., "Evaluation of Small Scale Icing Tunnel Test Results," SAE Technical Paper 2007-01-3328, 2007, https://doi.org/10.4271/2007-01-3328.Also In
References
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