[1] |
GAO Chuanqiang, ZHANG Weiwei.
Numerical simulation and modal analysis of transonic buffet flow over wings
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(7): 122597-122597.
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[2] |
WANG Ziyi, ZHANG Weiwei.
Unsteady aerodynamic reduced-order modeling method for parameter changeable structure
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(6): 220829-220829.
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[3] |
KOU Jiaqing, ZHANG Weiwei, GAO Chuanqiang.
Modal analysis of transonic buffet based on POD and DMD method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(9): 2679-2689.
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[4] |
ZHANG Weiwei, GAO Chuanqiang, YE Zhengyin.
Research advances of wing/airfoil transonic buffet
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(4): 1056-1075.
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[5] |
KOU Jiaqing, ZHANG Weiwei, YE Zhengyin.
Dynamic nonlinear aerodynamics modeling method based on layered model
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(12): 3785-3797.
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[6] |
GAO Chuanqiang, ZHANG Weiwei, YE Zhengyin.
Study on transonic buffet suppression with flapping rudder
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(10): 3208-3217.
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[7] |
XU Lincheng, WANG Gang, WU Jie, YE Zhengyin.
Uncertainty Analysis of Airfoil Wind Tunnel Tests with Automatic Differentiation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(8): 2102-2111.
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[8] |
TIAN Yun, LIU Peiqing, PENG Jian.
Using Shock Control Bump to Improve Transonic Buffet Boundary of Airfoil
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(8): 1421-1428.
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[9] |
LI Peifeng, ZHANG Binqian, CHEN Yingchun.
A Two-step Optimization Method of Transonic Wing Design for Engineering Application
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(12): 2153-2162.
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[10] |
XU Jianhua, SONG Wenping, HAN Zhonghua.
Prediction of Aeroacoustic Noise for Helicopter Rotors Based on Vorticity Confinement Method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(12): 2204-2212.
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[11] |
Shi Yongjie;Zhao Qijun;Xu Guohua.
Numerical Calculation and Parametric Study of Aerodynamics of Rotor Blade-vortex Interaction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(6): 1106-1114.
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[12] |
Li Jianbing;Wang Xuesong;Wang Tao.
Rapid Modeling of Distribution of Aircraft Wake Dielectric Constant Based on Horseshoe Vortex Model
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(7): 1214-1218.
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[13] |
Liu Chen;Wang Jiangfeng;Wu Yizhao.
Convergence Characteristics of Preconditioned Euler Equations at Low Mach Numbers
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(5): 842-848.
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[14] |
Lu Hongqiang;Wu Yizhao;Zhou Chunhua;Tian Shuling.
High Resolution of Subsonic Flows on Coarse Grids
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(2): 200-204.
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[15] |
Song Xizhen;Zhou Sheng;Li Qiushi.
Way of Improving Aerodynamic Load Coefficient of Transonic Axial Fan Rotor
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(1): 12-20.
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