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Numerical simulation of acoustic scattering and flow-induced noise with sharp interface immersed boundary method 会议论文
AIAA Scitech 2020 Forum, Orlando, FL, 2020/1/6-10
Authors:  Zhao C;  Yang Y(杨焱);  Zhang T;  Dong HB
Adobe PDF(1785Kb)  |  Favorite  |  View/Download：141/54  |  Submit date：2021/02/01
Shape design to minimize the peak heat-flux of blunt leading-edge 会议论文
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, Grapevine, TX, United states, JAN 07-10, 2013
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Cui K(崔凯)
View  |  Adobe PDF(605Kb)  |  Favorite  |  View/Download：652/313  |  Submit date：2014/02/24
Numerical analyses of discrete gust response for a flexible aircraft 会议论文
21st AIAA Applied Aerodynamics Conference 2003, Orlando, FL, United states, June 23, 2003 - June 26, 2003
Authors:  Yang GW(杨国伟);  Obayashi S
View  |  Adobe PDF(1991Kb)  |  Favorite  |  View/Download：197/85  |  Submit date：2017/06/01
Direct-coupling Method  Dynamic Equations Of Motion  Flexible Aircraft  Flexible Airplane  Freedom Of Motion  One-minus-cosine Gust  Quasi-steady Model  Supersonic Transport