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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    Titel :

    Computational Aerodynamic Design Tools and Techniques Used at Fighter Development


    Beteiligte:
    P. Sacher (Autor:in) / W. Kraus (Autor:in) / R. Kunz (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    54 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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