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Coupling mechanism analysis of a slender delta wing in combined freeroll and freesideslip motion
YANG Xiaoliang, LIU Wei, WU Tianzuo, LIU Xu
2014, 32(1): 1-7. DOI: 10.7638/kqdlxxb-2012.0072
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The design of osculating curved cone waverider based hypersonic vehicle
WU Yingchuan, HE Yuanyuan, HE Wei, LE Jialing
2014, 32(1): 8-13. DOI: 10.7638/kqdlxxb-2012.0054
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Crossflow instability analysis and transition prediction of airfoil boundary layer
HUANG Zhangfeng, LU Xuezhi, YU Gaotong
2014, 32(1): 14-20. DOI: 10.7638/kqdlxxb-2012.0062
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Numerical simulation of cross-flow around multiple-circular cylinders by spectral element method
HAN Zhaolong, ZHOU Dai, CHEN Yanan, GUI Xiaolan, LI Junlong
2014, 32(1): 21-29. DOI: 10.7638/kqdlxxb-2012.0070
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Optimization of sonicboom and aerodynamic based on structured/unstructured hybrid grid
FENG Xiaoqiang, LI Zhanke, SONG Bifeng, SANG Jianhua
2014, 32(1): 30-37. DOI: 10.7638/kqdlxxb-2012.0071
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Numerical investigation of jet interactions and optimization design of drag reduction for the afterbody of jet aircraft
XU Jia, CAI Jinsheng, LIU Qiuhong
2014, 32(1): 38-44. DOI: 10.7638/kqdlxxb-2012.0061
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The constant pressure time of piston driver in free piston shock tunnel
ZHU Hao, SHEN Qing, GONG Jian
2014, 32(1): 45-50. DOI: 10.7638/kqdlxxb-2012.0048
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Boundary layer correction for low speed wind tunnel contraction
LIU Weihong, HUANG Weimin
2014, 32(1): 51-56. DOI: 10.7638/kqdlxxb-2012.0066
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Research on the scaling law for the RCS of underdense turbulent wake of hypersonic vehicle
YU Zhefeng, BU Shaoqing, SHI Anhua, MA Ping, LIANG Shichang, HUANG Jie
2014, 32(1): 57-61. DOI: 10.7638/kqdlxxb-2012.0044
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The dual-wings terminal sensitive projectile bending angle effect on the aerodynamic characteristics
HU Zhipeng, LIU Rongzhong, GUO Rui
2014, 32(1): 62-68. DOI: 10.7638/kqdlxxb-2012.0043
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Study on the supersonic unsteady aerodynamic force for the morphing airfoil
GAO Yanfeng, LIU Zhifan, WANG Xiaohong
2014, 32(1): 69-76. DOI: 10.7638/kqdlxxb-2012.0056
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Optimal design of a new wind turbine blade based on performance and light weight
WANG Quan, , CHEN Jin, GUO Xiaofeng, LIN Songlin
2014, 32(1): 77-84. DOI: 10.7638/kqdlxxb-2012.0063
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Numerical analysis of wind turbine aerodynamic performance based on actuator line method
ZHU Chong, WANG Tongguang, ZHONG Wei
2014, 32(1): 85-91. DOI: 10.7638/kqdlxxb-2012.0042
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Numeric simulation and control optimization on missile trimmed flight
DA Xingya, TAO Yang, ZHAO Zhongliang, MA Xiaoyong
2014, 32(1): 92-95. DOI: 10.7638/kqdlxxb-2012.0045
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Suborbital reuse launch vehicle aerodynamic optimization method of layout
WANG Xugang, DU Tao, ZHANG Naimin
2014, 32(1): 96-100. DOI: 10.7638/kqdlxxb-2012.0046
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Study on multi-physical effects of hypersonic gliding waverider vehicles
HAN Hanqiao, ZHANG Chen′an, WANG Famin
2014, 32(1): 101-108. DOI: 10.7638/kqdlxxb-2012.0057
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Windtunnel test for galloping of iced quad bundle conductors
YAN Bo, LIU Xiaohui, HU Jing, ZHOU Song, ZHANG Hongyan
2014, 32(1): 109-115. DOI: 10.7638/kqdlxxb-2012.0064
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Construction and application research of HLL-HLLC scheme
FU Lin, GAO Zheng-hong, ZHANG Xiao-dong
2014, 32(1): 116-122. DOI: 10.7638/kqdlxxb-2012.0069
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The pneumatic energy analysis of typical bridge section wind induced vibration
LIU Zujun, YANG Yongxin, ZHOU Bingling
2014, 32(1): 123-130. DOI: 10.7638/kqdlxxb-2012.0047
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Effects of parameters on aerodynamic noise from wind turbine
SI Haiqing, WANG Tongguang, WU Xiaojun
2014, 32(1): 131-135. DOI: 10.7638/kqdlxxb-2012.0191
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