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- W808255119 abstract "Joint investigations have been carried out regarding the following problems: The atmospheric icing environment for modern transport aircraft; ice shapes and sizes on models in an icing wind tunnel; methods for making molds of ice; the effects of ice and hoar frost imitators on aerodynamic characteristics for a number of wing section and ice shapes, including advanced high lift devices; and flight tests for the determination of the effect of ice on flying characteristics. Icing effect prediction is discussed. Conclusions are presented which were reached from recent tests in a wind tunnel on a clean NACA 65A215 airfoil section as well as in a number of high-lift configurations with limited hoar frost and ice, and from flight tests. The findings indicate that: one must never ignore even slight icing; indications of the start of flow separation from the wind due to icing may be light buffeting of the aircraft, reduction of aileron control forces and roll disturbances; the development of flow separation from the wing due to icing is accelerated by a low landing approach speed and rough application of load factor larger than unity; the need for a timely activation of the anti-icing system." @default.
- W808255119 created "2016-06-24" @default.
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- W808255119 date "1977-10-01" @default.
- W808255119 modified "2023-09-23" @default.
- W808255119 title "AIRCRAFT ICING: STILL A SEVERE FLIGHT-SAFETY PROBLEM" @default.
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