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Recent development of high order DG/FV hybrid methods
ZHANG Laiping, LI Ming, LIU Wei, HE Xin, ZHANG Hanxin
2014, 32(6): 717-726. DOI: 10.7638/kqdlxxb-2014.0123
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Numerical optimization of flapping foil kinematics using high-order spectral difference method
YU Meilin, WANG Zhijian, HU Hui
2014, 32(6): 727-740. DOI: 10.7638/kqdlxxb-2014.0122
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Error analysis of high order schemes on non-uniform grids
WANG Qiuju, REN Yuxin
2014, 32(6): 741-747. DOI: 10.7638/kqdlxxb-2014.0108
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Numerical research of Cartesian based ghost cell method for compressible viscous flows
SHEN Zhiwei, ZHAO Ning, HU Ou
2014, 32(6): 748-754. DOI: 10.7638/kqdlxxb-2014.0105
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A dual platform theory for carbon based material oxidation with reaction diffusion rate controlled kinetics
GUO Yijun, DAI Guangyue, GUI Yewei, TONG Fulin, QIU Bo, LIU Bo
2014, 32(6): 755-760. DOI: 10.7638/kqdlxxb-2014.0047
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Calculating method of aerodynamic heating for hypersonic multi-body separation process
JI Weidong, WANG Jiangfeng, TANG Guoqing
2014, 32(6): 761-766. DOI: 10.7638/kqdlxxb-2014.0080
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Numerical study on hypersonic double cone separated flow
GONG Anlong, LIU Zhou, YANG Yunjun, ZHOU Weijiang
2014, 32(6): 767-771. DOI: 10.7638/kqdlxxb-2014.0083
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Heat flux estimation for heat transfer problem with ablation
QIAN Weiqi, ZHOU Yu, HE Kaifeng, SHAO Yuanpei
2014, 32(6): 772-776. DOI: 10.7638/kqdlxxb-2014.0038
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Application of data fusion technique in aerodynamics studies
HE Kaifeng, QIAN Weiqi, WANG Qing, KONG Yinan, WANG Wenzheng
2014, 32(6): 777-782. DOI: 10.7638/kqdlxxb-2014.0072
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Research on base flow field and aerodynamic characteristics of the supersonic base bleed projectile
ZHUO Changfei, FENG Feng, WU Xiaosong
2014, 32(6): 783-790. DOI: 10.7638/kqdlxxb-2013.0021
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Large eddy simulation of flow around a rectangular cylinder at low subsonic and transonic speeds
CHEN Jianping, HUANG Weixi, XU Chunxiao
2014, 32(6): 791-799. DOI: 10.7638/kqdlxxb-2013.0029
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Optimization of configuration and trajectory for hypersonic vehicles
FENG Yi, TANG Wei, GUI Yewei
2014, 32(6): 800-805. DOI: 10.7638/kqdlxxb-2013.0034
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Control of shock/boundary layer interaction in supersonic inlet using thermal excitation
YAN Hong, WANG Song
2014, 32(6): 806-813. DOI: 10.7638/kqdlxxb-2013.0102
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Investigation on internal weapon separation characteristics and flow control methods
WU Jifei, LUO Xinfu, XU Laiwu, FAN Zhaolin
2014, 32(6): 814-819. DOI: 10.7638/kqdlxxb-2012.0178
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Transonic wing aerodynamic design based on continuous adjoint method and free form deform technique
BAI Junqiang, CHEN Song, HUA Jun, SUN Zhiwei, HUANG Jiangtao
2014, 32(6): 820-826. DOI: 10.7638/kqdlxxb-2012.0198
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On the bistable phenomenon of a finite length square cylinder wake with POD method
WANG Hanfeng, XU Shengjin
2014, 32(6): 827-833. DOI: 10.7638/kqdlxxb-2012.0205
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Calculation of dynamic derivatives for aircraft based on CFD technique
MI Baigang, ZHAN Hao,
2014, 32(6): 834-839. DOI: 10.7638/kqdlxxb-2012.0206
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Extension of the delaunay tessellation particle tracking algorithm to 3D field
JIA Pan, WANG Yuan, ZHANG Yang, YANG Bin
2014, 32(6): 840-847. DOI: 10.7638/kqdlxxb-2012.0213
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Influence of the structural parameters on thermal performance of the hot air anti-icing system
PENG Long, BU Xueqin, LIN Guiping, MA Wentao, ZHAO Kai
2014, 32(6): 848-853. DOI: 10.7638/kqdlxxb-2012.0215
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Slat noise suppression based on upstream parallel mass injection
HUANG Hua, LI Weipeng, WANG Fuxin
2014, 32(6): 854-860. DOI: 10.7638/kqdlxxb-2012.0217
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Multi-field coupling numerical analysis approach for aerothermal environment of hypersonic vehicles
ZHANG Shengtao, CHEN Fang, LIU Hong
2014, 32(6): 861-867. DOI: 10.7638/kqdlxxb-2012.0220
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Effects of numerical method of source terms in turbulence models
WANG Xiangyu, LI Dong
2014, 32(6): 868-873. DOI: 10.7638/kqdlxxb-2012.0224
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