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- W41698896 abstract "Atmospheric icing presents a major hazard to aircraft operating under natural icing conditions and is a cause of major concerns for the certification authorities as well as the aircraft manufacturers. The steady rise in the global aviation traffic means an increased likelihood of encountering natural icing conditions. This suggests an increased frequency of icing related accidents unless a considerable amount of effort is focused on the various safety issues concerning in-flight aircraft icing, such as efficient design of ice protection related systems. To enhance flight safety under natural icing conditions, FAA has recently initiated a multi-year icing plan [1, 2] to address the various issues related to in-flight aircraft icing. One of the several key tasks outlined in the plan is the continued development of icing simulation methods to ensure their validity and reliability. In an effort to support the objectives of the FAA Icing Plan, and facilitate" @default.
- W41698896 created "2016-06-24" @default.
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- W41698896 date "2001-01-01" @default.
- W41698896 modified "2023-09-27" @default.
- W41698896 title "Ice Accretion Simulation Code CANICE" @default.
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