Continued studies have been undertaken to investigate and develop aerodynamic models that predict aircraft response in nonlinear unsteady flight regimes for transport configurations. The models retain conventional static and dynamic terms but replace conventional acceleration terms with indicial functions. In the Subsonic Fixed Wing Project of the NASA Fundamental Aeronautics Program and the Integrated Resilient Aircraft Controls project of the NASA Aviation Safety Program one aspect of the research is to apply these current developments to transport configurations to facilitate development of advanced simulation and control design technology. This paper continues development and application of a more general modeling methodology to the NASA Langley Generic Transport Model, a sub-scale flight test vehicle. In the present study models for the lateral-directional aerodynamics are developed.


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    Titel :

    Transport Aircraft System Identification Using Roll and Yaw Oscillatory Wind Tunnel Data


    Beteiligte:
    P. C. Murphy (Autor:in) / V. Klein (Autor:in)

    Erscheinungsdatum :

    2010


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Transport Aircraft System Identification Using Roll and Yaw Oscillatory Wind Tunnel Data

    Murphy, P. / Klein, V. | British Library Conference Proceedings | 2010



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    Transport Aircraft System Identification from Wind Tunnel Data

    Murphy, P. / Klein, V. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008