1–16 von 16 Ergebnissen
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    Unsteady Navier-Stokes Simulations of a Canard-Controlled Missile Configuration

    Sheng, C. / Wang, X. / Hughson, M. et al. | British Library Conference Proceedings | 2008

    Role of Laminar Length of Round Jet Impinging on Metal Foams

    Kuang, J. J. / Wang, X. L. / Lu, T. J. et al. | AIAA | 2015

    OTC 12969 Installation Method Evaluation of Export SCR's

    Wang, X. / Zhou, X. / Ginnard, A. J. et al. | British Library Conference Proceedings | 2001

    Modified Hilpert Correlation for Turbulent Convective Heat Transfer from a NACA Airfoil

    Wang, X. / Bibeau, E. / Naterer, G. F. | AIAA | 2007

      Modified Hilpert Correlation for Turbulent Convective Heat Transfer from a NACA Airfoil

      Wang, X. / Bibeau, E. / Naterer, G. et al. | British Library Conference Proceedings | 2007

    INCREMENTAL NONLINEAR CONTROL FOR AEROELASTIC WING LOAD ALLEVIATION AND FLUTTER SUPPRESSION

    Schildkamp, R. / Chang, J. / Sodja, J. et al. | TIBKAT | 2023

    Hammerstein model identification using quantum delta-potential-well-based particle swarm optimisation

    Du,Z. / Wang,X. / Henan Mechanical a.Electrical Engng.College,CN et al. | Kraftfahrwesen | 2011

    Dynamic modelling and stability analysis of articulated frame steer vehicles

    He,Y. / Khajepour,A. / McPhee,J. et al. | Kraftfahrwesen | 2005

    DEVELOPMENT OF AN ACTIVE AEROELASTIC PARAMETRIC WING APPARATUS

    Schildkamp, R. / Wang, X. / Chang, J. et al. | TIBKAT | 2023

    Convective Heat Transfer from a NACA Airfoil at Varying Angles of Attack

    Wang, X. / Naterer, G. F. / Bibeau, E. | AIAA | 2008