Method is developed to determine theoretical aerodynamic characteristics of VTOL-STOL aircraft; wing is represented by network of horseshoe vortices distributed on surface and trailing behind; jet efflux is represented with rectangular horseshoe vortex network in shape of curved tube; strength of each vortex segment is determined by requiring that flow be parallel to surface at number of control points; equations resolve into series of N equations with N unknowns that may be solved by computer using standard matrix inversion methods.


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    Titel :

    Method of representing fan-wing combinations for three-dimensional potential flow solutions


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Monical, R.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :