Aircraft icing

• Tuncer Cebeci ^[1] ; Fassi Kafyeke ^[2]
  1. [1] The Boeing Company, Long Beach, California, Estados Unidos
  2. [2] Bombardier Aerospace, Saint Laurent, Québec, Canada
• Localización: Annual review of fluid mechanics, ISSN 0066-4189, Nº. 35, 2003, págs. 11-21
• Idioma: inglés
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• Resumen

  • Full-scale icing experiments and, therefore, certification time and cost can be significantly reduced by developing calculation methods to evaluate the aircraft and system performance for a wide range of icing conditions. This article summarizes calculation methods for icing that include ice accretion, ice system performance, and icing effects on aircraft.