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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    Titel :

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


    Weitere Titelangaben:

    Springer Aerospace Techn.


    Beteiligte:
    Strelets, Dmitry Yu. (Herausgeber:in) / Korsun, Oleg N. (Herausgeber:in) / Suhanov, D. B. (Autor:in) / Serebryakov, L. I. (Autor:in) / Radchenko, P. A. (Autor:in) / Strijhak, S. V. (Autor:in)


    Erscheinungsdatum :

    2023-04-11


    Format / Umfang :

    15 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Forward swept wing flight demonstrator

    KRONE, JR., N. | AIAA | 1980



    Computations of Swept Wing Icing Aerodynamics

    Stebbins, Spencer J. / Loth, Eric / Qin, Chao | AIAA | 2019


    Carburetor icing demonstrator

    Rosenlund, I.T. | Engineering Index Backfile | 1957


    Swept wings in supersonic flight

    Gates, S. B. | TIBKAT | 1954