The basic processes of a program that performs sizing operations on a baseline aircraft and determines their subsequent effects on aerodynamics, propulsion, weights, and mission performance are described. Input requirements are defined and output listings explained. Results obtained by applying the method to several types of aircraft are discussed.


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    Title :

    Preliminary Sizing and Performance of Aircraft


    Contributors:

    Publication date :

    1985


    Size :

    120 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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