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Ice Accretion Effect on the Aerodynamic Characteristics of KC-100 Aircraft
2010
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
unpublished
In-flight icing is a serious hazard for flight safety. Ice accretion due to in-flight icing can affect the air flow of an aircraft; for example, it can increase drag, decrease lift, and degrade control authority. Thus, its effects must be checked during design and development by various methods such as theoretical analysis, icing wind tunnel experiments, and flight testing. Traditionally, icing simulation techniques based on the Lagrangian approach for droplet impingement and the potential flow
doi:10.2514/6.2010-1237
fatcat:b3qrwdlsenbz7p33ac3cm6ryre