A flight investigation of an automatic throttle control in landing approaches has been made. It was found that airspeed could be maintained satisfactorily by the automatic throttle control. Turbulent air caused undesirably large variations of engine power which were uncomfortable and disconcerting; nevertheless, the pilot felt that he could make approaches 5 knots slower with equal assurance when the automatic control was in operation.


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    Titel :

    Flight Investigation of an Automatic Throttle Control in Landing Approaches


    Beteiligte:

    Erscheinungsdatum :

    1959-03-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Flight Investigation of an Automatic Throttle Control in Landing Approaches

    L. J. Lina / R. A. Champine / G. J. Morris | NTIS | 1959


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