Configuration optimization, component design, and experimental proof in fighter design are summarized. Requirements for supersonic performance, including supersonic drag reduction and canard tail design, were reviewed. The main aerodynamic principles in use throughout the aircraft industry are described.


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    Title :

    Computational Aerodynamic Design Tools and Techniques Used at Fighter Development


    Contributors:
    P. Sacher (author) / W. Kraus (author) / R. Kunz (author)

    Publication date :

    1979


    Size :

    54 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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