[1] |
WU Hangkong, WANG Dingxi, HUANG Xiuquan, XU Shenren.
Influence of “frozen viscosity assumption” on solution and gradient accuracy of adjoint system
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(7): 125512-125512.
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[2] |
ZHANG Haoyuan, SUN Dong, QIU Bo, ZHU Yandan, WANG Anling.
Influence of turbulent kinetic energy on shock wave/boundary layer interaction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(7): 125504-125504.
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[3] |
SHU Bowen, DU Yiming, GAO Zhenghong, XIA Lu, CHEN Shusheng.
Numerical simulation of Reynolds stress model of typical aerospace separated flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526385-526385.
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[4] |
DU Yinjie, SHU Chang, YANG Liming, WANG Yan, WU Jie.
Wall model based diffuse-interface immersed boundary method and its application in turbulent flows
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726361-726361.
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[5] |
TONG Xin, QIANG Xiaoqing, YU Peixiang, OUYANG Hua.
Leading edge design method based on curvature distribution control
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124712-124712.
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[6] |
LI Chaoqun, LI Yi, ZHANG Chenxi, TANG Shuo.
Direct numerical simulation of flow field over streamwise micro riblets
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 123628-123628.
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[7] |
YUAN Xiangjiang, SHA Xinguo, SHI Xiaotian, GAO Jun.
Noise-turbulence relationship in hypersonic flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 123791-123791.
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[8] |
LIU Jingyuan.
Extension of field synergy principle for convective heat transfer to high speed compressible boundary-layer flows
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(1): 121429-121429.
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[9] |
ZOU Dongyang, LIU Jun, ZOU Li.
Applications of shock-fitting technique for compressible flow in cell-centered finite volume methods
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(11): 121363-121363.
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[10] |
WU Ziniu, BAI Chenyuan, XU Shanshu, LI Juan, LIN Jing, CHEN Zijun, YAO Yao.
Impulsively starting flow problem: from incompressible to hypersonic flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(8): 2588-2600.
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[11] |
XU Jiakuan, BAI Junqiang, QIAO Lei, HUANG Jiangtao, SHI Yayun.
Transition model for predicting crossflow instabilities
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(6): 1814-1822.
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[12] |
XU Changyue, ZHOU Tao, WANG Conglei.
Large Eddy Simulation of Flow in a Plane Supersonic Ejector
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(8): 2136-2143.
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[13] |
GAO Xinglong, TANG Qian'gang, ZHANG Qingbin, LI Jinhong.
Numerical Study on Fluid-structure Interaction of Slot-parachute’s Inflation Process
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(10): 2265-2276.
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[14] |
WANG Weixing, GUO Rongwei.
Study of Flow Characteristics of Hypersonic Inlet Based on Boundary Layer Transition
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(10): 1772-1780.
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[15] |
HUANG Jiangtao, GAO Zhenghong, BAI Junqiang, ZHAO Ke, LI Jing, XU Fang.
Laminar Airfoil Aerodynamic Optimization Design Based on Delaunay Graph Mapping and FFD Technique
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(10): 1817-1826.
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