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Display Method:
Support form and support interference on transport aircraft model in high speed wind tunnel
Yang Xianwen, Liu Xin
2015, 33(6): 721-727. DOI: 10.7638/kqdlxxb-2014.0064
Abstract PDF
A supercritical airfoil design based on multi-output surrogate model
Wu Kuanzhan, Liu Xuejun, Lyu Hongqiang
2015, 33(6): 728-732,746. DOI: 10.7638/kqdlxxb-2014.0059
Abstract PDF
Numerical analysis of BLU_SGS method in WCNS high-order scheme
Wang Guangxue, Zhang Yulun, Wang Yuntao, Li Song, Meng Dehong, Li Wei
2015, 33(6): 733-739. DOI: 10.7638/kqdlxxb-2014.0061
Abstract PDF
Study on forebody separation vortices using plasma actuations
Wang Jianlei, Meng Xuanshi, Li Huaxing, Liu Feng, Luo Shijun
2015, 33(6): 740-746. DOI: 10.7638/kqdlxxb-2014.0053
Abstract PDF
A highly-efficient predetermined boundary moving-embedded grid method suitable for the rotor CFD calculation
Li Peng, Zhao Qijun, Wang Bo
2015, 33(6): 747-756. DOI: 10.7638/kqdlxxb-2014.0057
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Optimization of suction control on separation flow around an airfoil at low Reynolds number
Zhang Wanglong, Tang Junjie, Chen Zhihua, Ren Dengfeng
2015, 33(6): 757-764. DOI: 10.7638/kqdlxxb-2014.0063
Abstract PDF
A new second-order bound-preserving conservative remapping algorithm in the ALE method
Li Zhenzhen, Yu Xijun, Jia Zupeng, An Na, Huang Chaobao
2015, 33(6): 765-771,786. DOI: 10.7638/kqdlxxb-2014.0078
Abstract PDF
The estimation of atmospheric parameters based on the airflow velocity over blunt sphere
Qian Lilin, Tao Jianwu, Yang Yueming, Yu Fei
2015, 33(6): 772-779. DOI: 10.7638/kqdlxxb-2014.0069
Abstract PDF
Experimental investigation on pressure loss of compressible combining flow at 45° T-junctions
Wang Wenhui, Lu Zhenhua, Deng Kangyao, Liu Sheng
2015, 33(6): 780-786. DOI: 10.7638/kqdlxxb-2014.0039
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Wind tunnel test on aerodynamic coefficients of multi-bundled sub-conductors
Lou Wenjuan, Li Tianhao, Lyu Zhongbin, Lu Ming
2015, 33(6): 787-792,817. DOI: 10.7638/kqdlxxb-2014.0056
Abstract PDF
Test particle Monte Carlo simulation for return flux due to ambient scatter of outgassing molecules on a circular disk
Jin Xuhong, Huang Fei, Cheng Xiaoli, Wang Qiang
2015, 33(6): 793-798. DOI: 10.7638/kqdlxxb-2014.0077
Abstract PDF
Numerical simulation of performance characteristics of two-electrode plasma synthetic jet and the influence of different actuator orifice shapes
Zhou Yan, Liu Bing, Wang Lin, Luo Zhenbing, Xia Zhixun
2015, 33(6): 799-805. DOI: 10.7638/kqdlxxb-2014.0037
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Numerical simulation of multi-element airfoil in unsteady ground effect
Zhu Yixi, Lu Zhiliang, Guo Tongqing
2015, 33(6): 806-811. DOI: 10.7638/kqdlxxb-2014.0048
Abstract PDF
Study of aerodynamic shape optimization for natural laminar wing
Ma Xiaoyong, Zhang Yanjun, Duan Zhuoyi, Guo Hongtao, Li Quan
2015, 33(6): 812-817. DOI: 10.7638/kqdlxxb-2014.0054
Abstract PDF
Test on launch jet noise of liquid rocket with single nozzle
Chen Jinsong, Zeng Lingfang, Hu Xiaowei, Fan Hong
2015, 33(6): 818-822. DOI: 10.7638/kqdlxxb-2014.0052
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Experimental investigation on flying wing lift enhancement and drag reduction by plasma
Yu Jinge, Niu Zhongguo, Liang Hua, Guan Jiaming, Hu Qiuqi
2015, 33(6): 823-827. DOI: 10.7638/kqdlxxb-2014.0055
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Simulation of plates group initial separation in high speed
Wang Zhengwei, Wang Hao, Ruan Wenjun, Ning Huijun, Wang Jinglong, Wang Pengxin
2015, 33(6): 828-834. DOI: 10.7638/kqdlxxb-2014.0076
Abstract PDF
The effect of trailing edge flaps length on aerodynamics of wind turbine airfoil
Han Zhonghe, Jia Yalei, Li Hengfan, Zhu Xiaoxun, Dong Shuai
2015, 33(6): 835-842. DOI: 10.7638/kqdlxxb-2015.0021
Abstract PDF