A new dynamic test mechanism has been developed in the unsteady low-speed wind tunnel at Nanjing University of Aeronautics and Astronautics to enhance the abilities of experiments in the unsteady flow cases. The structure of the new test mechanism is described in detail in this paper and the equations used to control the performance of test model's motions are also listed here. Then a wing-body model was tested in the new test system for the first time, including the forced oscillation tests and free-to-roll test at high angle of attack region. The test results are also discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A new hybrid mechanism for dynamic wind tunnel test of high maneuverable air vehicle




    Erscheinungsdatum :

    2016




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch



    Klassifikation :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik
    Lokalklassifikation TIB:    275/7040



    A new hybrid mechanism for dynamic wind tunnel test of high maneuverable air vehicle

    Geng, Xi / Shi, Zhiwei / Cheng, Keming et al. | SAGE Publications | 2016


    HIGHLY MANEUVERABLE VEHICLE

    MEAGER BENJAMIN | Europäisches Patentamt | 2023

    Freier Zugriff


    HIGHLY MANEUVERABLE VEHICLE

    MEAGER BENJAMIN | Europäisches Patentamt | 2023

    Freier Zugriff