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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1995, Vol. 16 ›› Issue (1): 34-38.

• 论文 • Previous Articles     Next Articles

HEAT LOAD CALCULATION FOR ANTI-ICING ON AIRCRAFT WINDSHIELD

Han Fenghua, Zuo Yansheng, Li Dongliang   

  1. Faculty 505 of Beijing University of Aeronautics and Astronautics, Beijing,100083
  • Received:1993-09-05 Revised:1994-02-21 Online:1995-02-25 Published:1995-02-25

Abstract: A brief summarizatio is made about the reasons and hazards of aircraft icing and the methods of anti-icing.A detail discussion and a method about the heat load calculating for anti-icing on aircraft windshield are presented.The results of this calculation method agree well with the available foreign data. The errors are within the range of ±5%. Therefore this calculation method can be used for engineering design.

Key words: heat - flux, aircraft icing, windshields

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