1–16 von 16 Ergebnissen
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    Courant Number Insensitive CE/SE Euler Scheme

    Chang, S. / Wang, X. | AIAA | 2002

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

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

    Nonlinear Structural Reduced Order Modeling Methods for Hypersonic Structures

    Matney, Andrew / Perez, R. / Spottswood, Stephen et al. | AIAA | 2012

    Measurements of a confined coaxial square jet

    Wang, X. / Yu, S. / Chua, L. | AIAA | 2002

    Numerical Simulation of Aluminized Propellants by a Level Set Method

    Wang, X. / Jackson, T. / Massa, L. | AIAA | 2003

    Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion

    Wang, X. / Van Kampen, E. / Chu, Q. P. et al. | AIAA | 2019

    Gust acoustic response of a single airfoil using the space-time CE/SE method

    Wang, X. / Chang, S. / Himansu, A. et al. | AIAA | 2002

    Three-Dimensional Modeling of Aluminized Composite Solid Propellant Combustion

    Wang, X. / Jackson, Thomas / Buckmaster, J et al. | AIAA | 2006

    Fast algorithms for 3-D fluid flow in micromachined devices

    Ye, W. / Kanapka, J. / Wang, X. et al. | AIAA | 2001

    Simulating turbulent flow over thin element and flat valley V-shaped riblets

    Pollard, A. / Tullis, S. / Wang, X. et al. | AIAA | 1996