SAE Technical Paper Series 2015
DOI: 10.4271/2015-01-2083
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Parametric Evaluation of Icing Effects by a Quasi-3D Methodology for High-Lift Configurations

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“…Aerofoil performance is also affected by small scale ice accretion; it increases the surface roughness and so trips the boundary layer. The effect of icing on high-lift configuration wings has been investigated by Sang et al [11], Bidwell [12] and Silva et al [13]. They all highlighted the critical situation of ice accumulating during hold, resulting in a loss of performance during descent, approach and landing, whilst the high-lift devices are deployed.…”
Section: Introductionmentioning
confidence: 99%
“…Aerofoil performance is also affected by small scale ice accretion; it increases the surface roughness and so trips the boundary layer. The effect of icing on high-lift configuration wings has been investigated by Sang et al [11], Bidwell [12] and Silva et al [13]. They all highlighted the critical situation of ice accumulating during hold, resulting in a loss of performance during descent, approach and landing, whilst the high-lift devices are deployed.…”
Section: Introductionmentioning
confidence: 99%