1–12 of 12 hits
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    Courant Number Insensitive CE/SE Euler Scheme

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

    Nonlinear Reduced Order Modeling of Complex Wing Models

    Wang, X. Q. / Perez, Ricardo A. / Mignolet, Marc P. | AIAA | 2013

    Nonlinear Structural Reduced Order Modeling Methods for Hypersonic Structures

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

    Issues in the Combustion of Aluminized Heterogeneous Propellants

    Wang, X / Jackson, Thomas / Buckmaster, John | AIAA | 2006

    Measurements of a confined coaxial square jet

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

    A Study of Fully Coupled 2D+ Airfoil FSI Models with Different FSI Approaches

    Wang, X. Sheldon / Gordnier, Raymond / Ji, S. et al. | AIAA | 2009

    Numerical Simulation of Aluminized Propellants by a Level Set Method

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

    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