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Shaoqiang HAN, Wenping SONG, Zhonghua HAN, Jianhua XU.
High-accuracy numerical-simulation of unsteady flow over high-speed coaxial rigid rotors
[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529064-529064.
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Li NONG, Zishuai SHENG, Jun XIAN, Huaibao ZHANG.
Numerical simulation of separated flow around iced airfoil based on high⁃order schemes
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729291-729291.
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WANG Di, QIAN Zhansen, LENG Yan.
High-order scheme discretization of sonic boom propagation model based on augmented Burgers equation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 124916-124916.
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QIU Zihua, XU Min, ZHANG Bin, LIANG Chunlei.
A parallel high-order method for simulating vortex-induced vibrations
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(3): 122483-122483.
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YAN Zhenguo, LIU Huayong, MAO Meiliang, MA Yankai, ZHU Huajun.
Development of 3rd-order HWCNS and its application in hypersonic flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(5): 1460-1470.
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TU Guohua, YAN Zhenguo, ZHAO Xiaohui, MA Yankai, MAO Meiliang.
SA and SST turbulence models for hypersonic forced boundary layer transition
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(5): 1471-1479.
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YAN Zhenguo, LIU Huayong, MAO Meiliang, DENG Xiaogang, ZHU Huajun.
Convergence Property Investigation of GMRES Method Based on High-order Dissipative Compact Scheme
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(5): 1181-1192.
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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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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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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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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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HUANG Ming-ke.
COMPUTATION OF THE FLOW PAST AIRCRAFT USING UNSTRUCTURED CARTESIAN GRID AND EULER EQUATIONS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2002, 23(6): 564-567.
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DONG Cheng-dong;YE Wei-guo.
RESEARCH ON AERODYNAMICAL CHARACTERISTICS OF A FIN WITH BULGE
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2002, 23(4): 324-326.
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Zhou Chunhua;Yang Zousheng.
ADAPTIVE FINITE ELEMENT METHOD FOR FULER EQUATIONS ON UNSTRUCTURED MESHES
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1994, 15(9): 1025-1031.
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Cai Qingdong;Wen Gongbi.
FINITE ELEMENTFLUX CORRECTED TRANSPORT(FEM-FCT)SOLUTION OF TWO-DIMENSIONAL EULER EQUATIONS ON AN ADAPTIVE TRIANGULAR MESH
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1994, 15(11): 1291-1297.
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