Minimum takeoff and landing distances are calculated and various effects considered at various thrust-to-weight ratios; it appears that takeoff to and landing from 50-ft obstacle can be achieved to 400 ft at all-up-weight 60% greater than VTO all-up weight.


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    Titel :

    Estimation of minimum field requirements of two overloaded, propeller-driven, tilt-wing VTOL aircraft (Including effects of flap setting, runway surface, wind, wing tilt rate and flap boundary layer control)


    Weitere Titelangaben:

    Canada. Nat Research Council -- Aeronautical Report


    Beteiligte:
    Neal, B. (Autor:in) / Lyster, H.N.C. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    41 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Tilt-wing VTOL aircraft

    McCormick, Jr., B.W. / Mallen, J. | Engineering Index Backfile | 1957


    Hybrid Tilt Propeller/Tilt Wing Aircraft

    WYGNANSKI ISRAEL / TAUBERT LUTZ / OL MICHAEL | Europäisches Patentamt | 2024

    Freier Zugriff

    Hybrid Tilt Propeller/Tilt Wing Aircraft

    WYGNANSKI ISRAEL / TAUBERT LUTZ / OL MICHAEL | Europäisches Patentamt | 2024

    Freier Zugriff

    Field requirements of overloaded propeller-driven VTOL aircraft

    Neal, B. / Lyster, H.N.C. | Engineering Index Backfile | 1963


    Tilt-wing propeller VTOL aircraft -- Present status and future role

    Mallen, J. / Dancik, P. | Engineering Index Backfile | 1959