1–20 von 35 Ergebnissen
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    A Study of Fully Coupled 2D+ Airfoil FSI Models with Different FSI Approaches

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

    Atomization performance of pressure-swirl nozzles

    WANG, X. / LEFEBVRE, A. | AIAA | 1986

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

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

    Courant Number Insensitive CE/SE Euler Scheme

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

    Fast algorithms for 3-D fluid flow in micromachined devices

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

    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

    Issues in the Combustion of Aluminized Heterogeneous Propellants

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

    Mean drop sizes from pressure-swirl nozzles

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

    Measurements of a confined coaxial square jet

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