A dynamic model was used to directly compare four different crosswind landing gear mechanisms. The model was landed as a free body onto a laterally sloping runway used to simulate a crosswind side force. A radio control system was used for steering to oppose the side force as the model rolled to a stop. The configuration in which the landing gears are alined by the pilot and locked in the direction of motion prior to touchdown gave the smoothest runout behavior with the vehicle maintaining its crab angle throughout the landing roll. Nose wheel steering was confirmed to be better than steering with nose and main gears differentially or together. Testing is continuing to obtain quantitative data to establish an experimental data base for validation of an analytical program that will be capable of predicting full scale results.


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    Titel :

    Model studies of crosswind landing-gear configurations for STOL aircraft


    Beteiligte:
    Stubbs, S. M. (Autor:in) / Byrdsong, T. A. (Autor:in)


    Erscheinungsdatum :

    01.10.1973


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Crosswind Landing Gear Position Indicator

    R. A. Champine | NTIS | 1977


    Crosswind landing-gear position indicator

    Champine, R. A. | NTRS | 1976



    Arrested Landing Studies for STOL Aircraft

    Chen-Chung Hsin | AIAA | 1974


    A predictive pilot model for STOL aircraft landing

    Kleinman, D. L. / Killingsworth, W. R. | NTRS | 1974