1998
DOI: 10.2514/2.472
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Modeling the Flow of Water on Aircraft in Icing Conditions

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Cited by 41 publications
(11 citation statements)
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“…The safety and performance of modern aircraft are significantly reduced even by light, scarcely visible ice on airfoils, compression inlets of air-breathing engines, and air flow measurement instruments. In-flight icing occurs mainly under certain weather conditions during the holding time before landing, usually at altitudes 9000−20 000 ft, when the aircraft exterior might be subjected to impact of supercooled water droplets present in the upper troposphere and cirrus clouds. , These droplets, which range in size , from 0 to 500 μm, collide with the cool skin of the aircraft and may cause ice accretion, thus compromising safety. In another example, ice buildup on wind turbine blades adversely affects blade aerodynamics, thus increasing drag and, in turn, robbing the energy output of the turbine.…”
Section: Introductionmentioning
confidence: 99%
“…The safety and performance of modern aircraft are significantly reduced even by light, scarcely visible ice on airfoils, compression inlets of air-breathing engines, and air flow measurement instruments. In-flight icing occurs mainly under certain weather conditions during the holding time before landing, usually at altitudes 9000−20 000 ft, when the aircraft exterior might be subjected to impact of supercooled water droplets present in the upper troposphere and cirrus clouds. , These droplets, which range in size , from 0 to 500 μm, collide with the cool skin of the aircraft and may cause ice accretion, thus compromising safety. In another example, ice buildup on wind turbine blades adversely affects blade aerodynamics, thus increasing drag and, in turn, robbing the energy output of the turbine.…”
Section: Introductionmentioning
confidence: 99%
“…Aiming at addressing the problem of flat water film flow, Myers et al [20,21] theoretically derived the prediction formula for continuous water film thickness. For the problem in this article, it can be simplified into a two-dimensional water film flow equilibrium height formula:…”
Section: Water Film Flow Equationmentioning
confidence: 99%
“…A flow model of the water film under aircraft icing condition has been derived by Myers [30,31], in which multiple effect factors are obtained, including ambient pressure, surface tension, gravity and shear stress. Myers' model was then applied in glaze icing, runback ice ridge and anti-icing simulations [32,33,34,35].…”
Section: Introductionmentioning
confidence: 99%
“…Mean film thickness under different (a) wind speed Ua and (b) film Reynolds number Ref. Schematic diagram of water film flow modelA formula for predicting the thickness of a continuous water film on aircraft in icing conditions was first derived theoretically by Myers[30,31], assuming that the film flow was stable. The model clarified the relationship between the interfacial shear stress and the equilibrium film thickness.…”
mentioning
confidence: 99%