Computational aerodynamics has evolved to be a practical design tool comparable to wind tunnel testing, and it has played an important role in actual aircraft design stages. There have been intensive works already done for code validation to support the accuracy of the computation. The code accuracy based upon comparison between numerical simulation and actual flight test is discussed for the first time.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Comparative Study on Wing Pressure Distribution of High Speed Jet Airplane Between Numerical Simulation and Flight Test


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

    Erscheinungsdatum :

    1989


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Airplane configurations for high speed flight

    Johnson, C.L. | Engineering Index Backfile | 1954


    FLIGHT TEST RESULTS FOR AN ADVANCED TECHNOLOGY LIGHT AIRPLANE WING

    Kohlman, David L. | SAE Technical Papers | 1974


    Airplane configurations for high speed flight

    Johnson, C.L. | Engineering Index Backfile | 1953


    Airplane configurations for high speed flight

    Johnson, C.L. | Engineering Index Backfile | 1953