As part of a program to investigate the fluctuating pressure distribution and response behavior of a fighter aircraft in transonic maneuver, an F-5A scale model has previously been tested in an 11-ft transonic wind tunnel. The model, with a number of static and dynamic pressure transducers imbedded in the lifting surfaces was tested at various angles of attack up to 16 deg. In this paper, test results of particular interest to wake flow and horizontal tail buffet are described. It is shown that the dynamic pressure data on the tail surface at the specified flight conditions serve to determine the local dynamic loads. They also influence the control performance of the aircraft under maneuver conditions where buffet is encountered. The data presented demonstrate a number of contributing factors that affect the tail dynamic pressures in the transonic regime.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aircraft wake flow effect and horizontal tail buffet


    Beteiligte:
    Hwang, C. (Autor:in) / Pi, W. S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1979-04-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aircraft Wake Flow Effect and Horizontal Tail Buffet

    Chintsun Hwang / W.S. Pit | AIAA | 1979


    Method to Analyze Tail Buffet Loads of Aircraft

    A. S. Pototzky / R. W. Moses | NTIS | 2005


    ANTI-TAIL BUFFET SYSTEM

    SMITH MICHAEL REAUGH / CHOI JOUYOUNG JASON | Europäisches Patentamt | 2020

    Freier Zugriff

    Transonic Tail Buffet Simulations on the ATRA Research Aircraft

    Illi, Sebastian A. / Lutz, Thorsten / Krämer, Ewald | Springer Verlag | 2013


    Transonic Tail Buffet Simulations on the ATRA Research Aircraft

    Illi, S.A. / Lutz, T. / Kramer, E. | British Library Conference Proceedings | 2013