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Li,Y., Shock, R., Zhang, R. and Chen, H., “Simulation of Flow over Iced Airfoil by Using a Lattice Boltzmann Method,”
AIAA Paper 2005-1103, 43rd AIAA Aerospace Sciences Meeting and Exhibit, January 10-13 2005, Reno, Nevada
Shock, R., Mallick, S., Chen, H., Yakhot, V., and Zhang, R., “Recent Simulation Results on 2D NACA Airfoils using a
Lattice Boltzmann Based Algorithm,” AIAA J. of Aircraft, Vol. 39, No.3, 2002, pp. 434-439.
AIAA-2008-4145-806增升装置气动噪音
AIAA-2008-549 多段翼型
AIAA-2008-3048-427机翼气动噪音
AIAA-2008-2916-677起落架噪音
AIAA 2008-34 Computational Aeroacoustics Analysis of a High-Lift Configuration
AIAA 2008-749 Lattice Boltzmann Simulations of the DLR-F4, DLR-F6 and Variants |
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