The study of aerodynamics has been preoccupied with understanding flight at increasing speeds and ultimately supersonic. Today, this pursuit has advanced the science for both Hypersonic and Transonic flight to near Mach 1 supporting economical commercial flight operations. This research presents the data from a Taguchi array on low speed with twin wing designs to establish the design parameters for their use in low speed and high altitude. Also presented is how aerodynamic advantages can be achieved through understanding the interactions of parameters and their use. This is compared to operational effectiveness when applied to remotely piloted aircraft that are not constrained by direct requirements. The research concludes with suggestions for improved designs and further work that may enable higher altitudes with low speeds.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic Analysis of Low Speed Wing Design using Taguchi L9 Orthogonal Array


    Beteiligte:
    Witcher Kenneth (Autor:in) / McAndrew Ian (Autor:in) / Vishnevskaya Elena (Autor:in)


    Erscheinungsdatum :

    2018




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




    Aerodynamic Design — Wing

    Emerald Group Publishing | 1969


    Aerodynamic Analysis of Low-Speed Wing-Flap Systems

    Carlson, H. W. / Walkley, K. B. | NTRS | 1985


    Aircraft wing design at low speeds using Taguchi method

    Soylak, Mustafa / Karagöz Gökçe, Nurseda / Topal, Eyüp Sabri | Emerald Group Publishing | 2018



    Nonlinear Aerodynamic Wing Design

    E. Bonner | NTIS | 1985