This paper reports the extension of the stress wave force balance to the measurement of forces on models which are non-axisymmetric or which have non-axisymmetric load distributions. Recent results are presented which demonstrate the performance of the stress wave force balance for drag measurement, for three-component force measurement and preliminary results for thrust measurement on a two-dimensional scramjet nozzle. In all cases, the balances respond within a few hundred microseconds.


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    Titel :

    Lift, drag and thrust measurement in a hypersonic impulse facility


    Beteiligte:
    Tuttle, S. L. (Autor:in) / Mee, D. J. (Autor:in) / Simmons, J. M. (Autor:in)

    Kongress:

    AIAA Aerospace Ground Testing Conference ; 1994 ; Colorado Springs, CO, United States



    Erscheinungsdatum :

    01.01.1995


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Lift, drag and thrust measurement in a hypersonic impulse facility

    Tuttle, S. / Mee, D. / Simmons, J. | AIAA | 1994


    Lift, Drag and Thrust Measurement in a Hypersonic Impulse Facility

    Tuttle, S. L. / Mee, D. J. / Simmons, J. M. et al. | British Library Conference Proceedings | 1994


    Measurement of Scramjet Nozzle Thrust in a Hypersonic Impulse Facility

    Tuttle, S. L. / Simmons, J. M. / Mee, D. J. et al. | British Library Conference Proceedings | 1995


    Maximizing Lift-to-Drag and Thrust-to-Drag Ratios for Trimmed Hypersonic Vehicles

    Mbagwu, Chukwuka C. / Dalle, Derek J. / Driscoll, James F. | AIAA | 2023