A computer study was made of the lateral response of a T-33 aircraft cruising at 450 mph true air speed at 35000 feet with tip tanks empty using a Summers 1025A Pilot Assist System. Studies of required gains and tilt angle were conducted. (Author)


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    Title :

    Computer Study of the Lateral Response of a T-33 Aircraft Using a Simulated Summers 1025A Pilot Assist System


    Contributors:

    Publication date :

    1954


    Size :

    52 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English