2017
DOI: 10.2514/1.b36067
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Experimental Investigation on Anti-Icing Performance of an Engine Inlet Strut

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Cited by 14 publications
(3 citation statements)
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“…Eighteen groups of examples were calculated in the study. The inflow parameters were selected based on actual flight conditions of civil aircraft and the range of ice accumulation parameters were provided by icing wind tunnel data [10,18]. In our study, since the water droplet size of 16μm was small, and no account was taken of droplet rebound and splash phenomena, the water droplets were assumed to stick to the spinner surface after droplet impact.…”
Section: Effect Of Spinner Shape On Droplet Impact Characteristicsmentioning
confidence: 99%
See 1 more Smart Citation
“…Eighteen groups of examples were calculated in the study. The inflow parameters were selected based on actual flight conditions of civil aircraft and the range of ice accumulation parameters were provided by icing wind tunnel data [10,18]. In our study, since the water droplet size of 16μm was small, and no account was taken of droplet rebound and splash phenomena, the water droplets were assumed to stick to the spinner surface after droplet impact.…”
Section: Effect Of Spinner Shape On Droplet Impact Characteristicsmentioning
confidence: 99%
“…Ahn et al [9] numerically and experimentally demonstrated that droplet size has a great influence on icing, and its influence increases with the growth of the droplet size at the air intake of a rotorcraft. W. Dong et al [10] used a wind tunnel to measure the main characteristics of ice growth and ice type under different temperature, inflow velocity and water content conditions on engine inlet lips. Experimental results showed that water flow patterns, temperature distribution and ice shapes are depended on the parameter of freestream.…”
Section: Introductionmentioning
confidence: 99%
“…Icing is one common aviation danger that plagues both unmanned and manned aircraft flying in cold climate. Aircraft icing occurs when small, supercooled, airborne water droplets freeze upon impacting an airframe surface that allows formation of ice [2][3][4]. The freezing can be complete or partial, depending on how rapidly the latent heat of fusion can be released into the ambient air.…”
mentioning
confidence: 99%