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    A High Order Cut-Cell Method for Numerical Simulation of Hypersonic-Boundary Transition with Arbitrary Surface Roughness

    Duan, L. / Wang, X. / Zhong, X. et al. | British Library Conference Proceedings | 2009

    AIAA 2006-1107 Numerical Simulation and Experiment Comparison of Leading-Edge Receptivity of A Mach 5.92 Boundary Layer

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006

    AIAA 2006-1108 Direct Numerical Simulation and the Theory of Receptivity in a Hypersonic Boundary Layer

    Tumin, A. / Wang, X. / Zhong, X. et al. | British Library Conference Proceedings | 2006

    DEVELOPMENT AND VALIDATION OF A HIGH-ORDER SHOCK-FITTING NON-EQUILIBRIUM FLOW SOLVER

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    DNS OF STRONG SHOCK AND TURBULENCE INTERACTIONS INCLUDING REAL GAS EFFECTS

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    DNS OF STRONG SHOCK AND TURBULENCE INTERACTIONS WITH THERMOCHEMICAL NON-EQUILIBRIUM EFFECTS

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    Effect of Compressibility on Strong Shock and Turbulence Interactions

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    Effect of Porous Coating and its Location on Hypersonic Boundary Layer Waves

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009

    EFFECT OF POROUS COATING ON BOUNDARY-LAYER INSTABILITY

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010

    Finite Roughness Effect on Modal Growth of a Hypersonic Boundary Layer

    Fong, D. / Wang, X. / Zhong, X. et al. | British Library Conference Proceedings | 2012

    NUMERICAL SIMULATION AND THEORETICAL ANALYSIS ON HYPERSONIC BOUNDARY-LAYER RECEPTIVITY TO WALL BLOWING-SUCTION

    Tumin, A. / Wang, X. / Zhong, X. et al. | British Library Conference Proceedings | 2010

    Numerical Simulation of Hypersonic Boundary-Layer Receptivity to Two and Three-Dimensional Wall Perturbations AIAA Paper

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007

    NUMERICAL SIMULATIONS ON MODE S GROWTH OVER FELTMETAL AND REGULAR POROUS COATINGS OF A MACH 5.92 FLOW

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    PHASE ANGLE OF POROUS COATING ADMITTANCE AND ITS EFFECT ON BOUNDARY-LAYER STABILIZATION

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    Receptivity of a Hypersonic Flat-Plate Boundary Layer to Surface Roughness

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

    Receptivity of a Supersonic Boundary Layer Over a Sharp Wedge to Wall Blowing/Suction

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004

    Stabilization of Hypersonic Boundary Layer Waves Using 2-D Surface Roughness

    Fong, K.D. / Wang, X. / Zhong, X. et al. | British Library Conference Proceedings | 2013

    THERMOCHEMICAL NON-EQUILIBRIUM EFFECTS ON PASSIVE CONTROL OF HYPERSONIC BOUNDARY-LAYER TRANSITION USING REGULAR POROUS COATING

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    The Stabilization of a Mach 10 Boundary Layer Using Regular Porous Coating

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

    TRANSIENT GROWTH OF A MACH 5.92 FLAT-PLATE BOUNDARY LAYER

    Wang, X. / Zhong, X. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010