Possibility of preparing chart for circling flight at any inclination of flight path; three equations for description of flight path may be derived on simple assumption that thrust acts almost along direction of flight, i.e., that angles of attack and of sideslip are negligibly small.


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    Title :

    Chart for steady circling flight


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Sponder, E. (author)

    Published in:

    Publication date :

    1955


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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