This paper describes the method for calculation of anti-icing system for swept wing of supersonic flight demonstrator X-59. The section heating elements on top and bottom surfaces of wing were defined using iceFoam solver and engineering method. The calculations showed that the total electric power to ensure the operation of the anti-icing system is equal to N = 13 081 Wt. The efficiency factor characterizing transformation process of electrical energy into heat is equal to about 0.88–0.95.


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    Title :

    To the Problem of Selecting the Anti-Icing System for the Swept Wing of Supersonic Flight Demonstrator


    Additional title:

    Springer Aerospace Techn.




    Publication date :

    2023-04-11


    Size :

    15 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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