Preliminary results are presented of a study conducted to analyze the effects of several plan-form modifications on the aerodynamic characteristics of a high-aspect-ratio, natural laminar flow (NLW) wing. The study addresses the potential aerodynamic improvements available at both cruise and high angles of attack by use os swept wing-tip shapes. The swept wing tip appears to offer a viable addition to the lift of wing-tip designs which provide improvements in aerodynamic efficiency, with the added safety benefit of providing high angle-of-attack departure resistance.


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    Titel :

    Swept wing-tip shapes for low-speed airplanes


    Beteiligte:
    Van Dam, C. P. (Autor:in)

    Erscheinungsdatum :

    01.10.1985


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Swept Wing-Tip Shapes for Low-Speed Airplanes

    van Dam, C. P. | SAE Technical Papers | 1985


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    DeYoung, John / Barling, Walter H. | TIBKAT | 1955


    Forward Swept Wings and Business Airplanes

    Roskam, Jan | SAE Technical Papers | 1980