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Display Method:
Development of a morphing wing with adaptive capability
LI Jun, QIN Yan-hua, BAI Tao, YU Zhe-hui, LI Yan
2009, 27(5): 505-508.
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Parallel algorithm for the simulation of 3D muzzle brake flow field
ZHANG Hui, TAN Jun-jie, CUI Dong-ming, WANG Xue-de, SHI Qing
2009, 27(5): 509-515.
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A study of the transition prediction of hypersonic boundary layer on plane and wedge flow
CAO Wei
2009, 27(5): 516-523.
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Aerodynamic data fusion technique exploration
WANG Wen-zheng, GUI Ye-wei, HE Kai-feng, YUAN Xian-xu, CHEN Yan-qin
2009, 27(5): 524-528.
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The effect of critical Reynolds number and zonal characteristics on asymmetric vortices at forebody
BO Nan, DENG Xue-ying, MA Bao-feng, WANG Yan-kui
2009, 27(5): 529-535.
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Numerical simulation of disturbance evolution in the boundary layer of a hypersonic blunt cone at low incidence
TU Guo-hua, YUAN Xiang-jiang, TAO Jian-jun, LU Li-peng
2009, 27(5): 536-541.
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The test technique for aircraft with high aspect ratio in the 2.4 meter transonic wind tunnel
CHEN De-hua, YIN Lu-ping, WU Wen-hua, LI Jian-qiang, SHI Jian-yuan, PENG Yun
2009, 27(5): 542-546.
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Analysis for second order time accurate CFD/CSD coupled algorithms
AN Xiao-min, XU Min, CHEN Shi-lu
2009, 27(5): 547-552.
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The comparison of design wind load parameters under complex terrain conditions in typhoon-prone region
ZHOU Yu-fen, ZHAO Lin, ZHU Le-dong, GE Yao-jun
2009, 27(5): 553-560.
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The effects of trailing edge jets on the vortex breakdown location over a delta wing
YAN Chao, ZHOU Yu, XIE Zi-xian, CHEN Yu
2009, 27(5): 561-565.
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Implicit algorithms for viscous flow simulation at arbitrary Mach number
SHI Wan-li, GE Ning, SHENG Chun-hua
2009, 27(5): 566-571.
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Wind press distribution characteristics analysis of long-span cantilevered curve roof in wind tunnel test
XIAN Rong, LIAO Hai-li, LI Ming-shui
2009, 27(5): 572-577.
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Application of CFD method to achieve the fluid field of an "Infinite Swept Wing" in wind tunnel
ZUO Sui-han, YANG Yong, LI Dong
2009, 27(5): 578-581.
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Numerical simulation of viscous flow-fields around helicopter rotor
MOU Bin, XIAO Zhong-yun, ZHOU Zhu, CHEN Zhuo-bing
2009, 27(5): 582-585.
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Reconstruction & prediction of wind pressure on heliostat
WANG Ying-ge, LI Zhen-gnong, GONG Bo, Li Qiu-sheng
2009, 27(5): 586-591.
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Store separation simulation using overset unstructured grid
TANG Zhi-gong, LI Bin, ZHENG Ming, DENG You-qi
2009, 27(5): 592-596.
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Effects of endwall relative motion on tip clearance flow in turbine rotors
NIU Mao-sheng, ZANG Shu-sheng
2009, 27(5): 597-601.
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Numerical experiments using one high-resolution scheme for unsteady inviscid compressible flows
XU Li, YANG Ai-ming, GUAN Peng, WENG Pei-fen
2009, 27(5): 602-607.
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The mutilgrid method in Euler equation computation about a helicopter rotor in hover
YANG Xiao-Quan, YANG Ai-Ming, WENG Pei-fen
2009, 27(5): 608-615.
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The partition to the fighter configuration
ZHANG Ji-gao
2009, 27(5): 616-622.
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