2019
DOI: 10.1016/j.coldregions.2019.01.012
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Analysis and modelling of icing of air intake protection grids of aircraft engines

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Cited by 19 publications
(9 citation statements)
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“…Preventing ice buildup on aerodynamic components is of primary importance to flight safety [1,2]. Ice accumulates especially on the front components of an aircraft, severely limiting its performance by increasing drag and decreasing lift.…”
Section: Introductionmentioning
confidence: 99%
“…Preventing ice buildup on aerodynamic components is of primary importance to flight safety [1,2]. Ice accumulates especially on the front components of an aircraft, severely limiting its performance by increasing drag and decreasing lift.…”
Section: Introductionmentioning
confidence: 99%
“…Ice accumulation can damage locks and dams [1], reduce the performance of cryogenic, refrigeration and air conditioning systems [2], cause power lines and telecommunication equipment outage [3]. Furthermore, ice accretions may result in dangerous road conditions and serious hazards during flights [4,5].…”
Section: Introductionmentioning
confidence: 99%
“…This ice accretion changes the airfoil geometry, altering the wing's aerodynamic characteristics (loss of lift, increase in drag). Icing conditions also threaten aircraft's engines with uncontrolled ice shedding and with air intakes protection grids icing, inducing power loss and eventually, causing engine flame-out in the case of total obstruction (Vercillo et al, 2019). Conventional thermal ice protection systems, such as hot air bleed systems (Moir and Seabridge, 2011) or more recent electro-thermal (bleed less) types, do require high power supply (Meier and Scholz, n.d.;Shinkafi and Lawson, 2014).…”
Section: Introduction and Objectivesmentioning
confidence: 99%