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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    Title :

    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)


    Additional title:

    Canada. Nat Research Council -- Aeronautical Report


    Contributors:
    Neal, B. (author) / Lyster, H.N.C. (author)


    Publication date :

    1963


    Size :

    41 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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