The identification of multi-input, single output linear static models from flight test data is discussed. Models based on least squares are considered. Wind tunnel scale model and flight test data on a propeller slipstream are compared. Dynamic flight test data were analyzed by reconstructing the flight path and forming a data base for the identification of aerodynamic models. Given the relatively low Reynolds number of the wind tunnel experiments, a reasonable correspondence exists between the dynamic flight test results and model predictions.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic Model Identification from Dynamic Flight Test Data and Wind Tunnel Experiments


    Beteiligte:
    J. A. Mulder (Autor:in) / J. G. Denhollander (Autor:in) / H. Binkhorst (Autor:in)

    Erscheinungsdatum :

    1982


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aerodynamic model identification from dynamic flight test data and wind tunnel experiments

    Mulder, J.A. / Hollander, J.G. den / Binkhorst, H. | Tema Archiv | 1982


    Aerodynamic Model Identification from Dynamic Flight Test Data and Windtunnel Experiments

    J. A. Mulder / J. G. den Hollander / H. Binkhorst | NTIS | 1982


    Model wind tunnel virtual flight test aerodynamic coefficient measurement method

    SHEN YANJIE / FENG SHUAI / WANG YANLING et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Two-point Aerodynamic Model Identification from Dynamic Wind Tunnel Tests

    Dias, Joaquim N. / Girardi, Roberto D. | AIAA | 2016