The generalized equations are discussed which pertain to an airplane executing its flight path in a single vertical plane, under a sequence of stipulations specifying the nature of the local optima which are distinctly different in character along successive portions of this path. The aerodynamic and propulsive characteristics of the airplane are allowed to be specified with complete generality.


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    Title :

    Optimum Airplane Flight Paths


    Contributors:
    P. Cicala (author)

    Publication date :

    1959


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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