Based on testing results of aerodynamic forces and pressures from a wind tunnel, the longitudinal aerodynamics characteristics of a forward swept wing are discussed in this paper. The results are also compared with the data of an associated aft swept wing. Measures of improving the inboard flowfield of a forward swept wing are also investigated, and the results are discussed. Under a low speed situation, an appropriate sweptback of the root section can improve the flow consequently obtaining higher aerodynamic performances.


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    Titel :

    Experiment Investigation on Longitudinal Characteristics of the Forward Swept Wing


    Beteiligte:
    Y. Guo (Autor:in) / X. Wang (Autor:in) / B. Zhang (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    29 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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