Various measurements concerning unsteady aerodynamics are discussed. The unsteady pressure measurements in a wing, used as points of comparison for the unsteady aerodynamic computation methods on which flutter computations are based, are mentioned and wind tunnel tests of flutter are analyzed. Various measurements, their use, and the safety systems are discussed to give an overview of what can be done in this area.


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    Titel :

    Unsteady Wind Tunnel Tests


    Beteiligte:
    P. M. Hutin (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    38 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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