Computational aerodynamics has evolved to the point where it has become a practical design tool comparable to wind tunnel testing and has played an important role in actual aircraft design stages. The Navier-Stokes code, however, is still restricted to two-dimensional applications, which have been repeatedly validated. The three-dimensional application, which is a real challenge for the Navier-Stokes code, is discussed. If this three-dimensional application could be perfected, it would be a big step toward the final target of complete aircraft analysis by numerical simulation.


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    Titel :

    Numerical Simulation of Transonic Aircraft in Comparison to Wind Tunnel Test


    Beteiligte:
    J. Miyakawa (Autor:in) / S. Takanashi (Autor:in) / K. Fujii (Autor:in) / K. Amano (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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