Aircraft icing flight research was performed in natural icing conditions with a twin engine computer type STOL aircraft. In-flight measurements were made of the icing cloud environment, the shape of the ice accretion on the wing, and the corresponding increase in the wing section drag. Results are presented for three icing encounters. On one flight, the wing section drag coefficient increased 35 percent over the uniced baseline for cruise conditions while a 43 percent increase was observed at an aircraft angle of attack of 6.2 degrees.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    In-Flight Measurements of Wing Ice Shapes and Wing Section Drag Increases Caused by Natural Icing Conditions


    Beteiligte:
    K. Mikkelsen (Autor:in) / N. Juhasz (Autor:in) / R. Ranaudo (Autor:in) / R. Mcknight (Autor:in) / R. Freedman (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    27 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Drag measurements on a junckers wing section

    Weidinger, H. | Engineering Index Backfile | 1926


    Rotary wing icing

    Mazonson, B.P. | Engineering Index Backfile | 1946


    Wing icing studies

    Online Contents | 1994


    Wing anti-icing and de-icing control power distribution device for fixed-wing aircraft

    FENG ZHIYUAN / WANG DA / QI ZEJUN et al. | Europäisches Patentamt | 2024

    Freier Zugriff