1–20 von 28 Ergebnissen
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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

    Mean drop sizes from pressure-swirl nozzles

    LEFEBVRE, A. H. / WANG, X. F. | AIAA | 1987

    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

    Turbulent Round Jet Control Using Two Steady Minijets

    Zhou, Y. / Du, C. / Mi, J. et al. | AIAA | 2012

    Reduced-Order Nonlinear Damping Model: Formulation and Application to Postflutter Aeroelastic Behavior

    Wang, X. Q. / Song, Pengchao / Mignolet, Marc P. et al. | AIAA | 2021

    Flexible Aircraft Gust Load Alleviation with Incremental Nonlinear Dynamic Inversion

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

    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

    Reduced Order Modeling with Local Enrichment for the Nonlinear Geometric Response of a Cracked Panel

    Wang, X. Q. / O’Hara, P. J. / Mignolet, M. P. et al. | AIAA | 2018

    Spray characteristics of aerated-liquid pressure atomizers

    LEFEBVRE, A. H. / WANG, X. F. / MARTIN, C. A. | AIAA | 1988