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Display Method:
Airflow control by NS-SDBD plasma actuators
MENG Xuanshi, SONG Ke, LONG Yuexiao, LI Huaxing
2018, 36(6): 901-916. DOI: 10.7638/kqdlxxb-2018.0078
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Mechanism and algorithm for geometric conservation law in finite difference method
LIU Jun, HAN Fang, XIA Bing
2018, 36(6): 917-926. DOI: 10.7638/kqdlxxb-2018.0034
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Weight and size estimation method of two-stage-to-orbit reusable launch vehicles
LIU Lei, YANG Xiaofeng, XIAO Guangming, WEI Dong, TANG Wei
2018, 36(6): 927-933. DOI: 10.7638/kqdlxxb-2018.0075
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Research of Reynolds number correction for supercritical wing based on wind tunnel tests and numerical simulations
ZHANG Yanjun, DUAN Zhuoyi, WEI Jianlong, LEI Wutao, ZHAO Ke
2018, 36(6): 934-940. DOI: 10.7638/kqdlxxb-2017.0213
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Multi-objective wing optimization of civil aircrafts in engine-aircraft integration configuration
XUE Bangmeng, ZHANG Wensheng, ZHANG Zhixiong
2018, 36(6): 941-948. DOI: 10.7638/kqdlxxb-2016.0126
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Effects of turbulence on galloping iced 8-bundled conductor
XU Qian, CAI Mengqi, ZHOU Linshu, YAN Bo, WANG Qingyuan
2018, 36(6): 949-957. DOI: 10.7638/kqdlxxb-2018.0045
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Numerical investigation of ice density effects on airfoil de-icing process
LEI Guilin, ZHENG Mei, DONG Wei, GUO Zhiqiang
2018, 36(6): 958-965. DOI: 10.7638/kqdlxxb-2016.0144
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Wind-induced vibration response analysis of high-rise lattice structure by considering modification effect for three-dimensional spatial and nonlinear vibration mode shape
WU Jiurong, ZHONG Wenkun, XU An
2018, 36(6): 966-973. DOI: 10.7638/kqdlxxb-2017.0111
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Applications of reduced reaction mechanism for numerical calculations in supersonic combustion of kerosene fuel
FAN Xiaofeng, WANG Jiangfeng, ZHAO Faming, YANG Tianpeng
2018, 36(6): 974-982. DOI: 10.7638/kqdlxxb-2017.0189
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Progress and prospects on aeroelasticity of hypersonic vehicles
YE Zhengyin, MENG Xianzong, LIU Cheng, YE Liuqing
2018, 36(6): 984-994. DOI: 10.7638/kqdlxxb-2018.0060
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A survey of aeroelastic wind tunnel test techonlogy of flight vehicles
YANG Ximing, LIU Nan, GUO Chengpeng, ZHANG Ying, SUN Jian, ZHANG Ge, YU Xianpeng, YU Jin'ge, HOU Liangxue
2018, 36(6): 995-1008. DOI: 10.7638/kqdlxxb-2018.0039
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Development of aerodynamic methods in aeroelastic analysis for high aspect ratio flexible wings
YANG Chao, YANG Lan, XIE Changchuan
2018, 36(6): 1009-1018. DOI: 10.7638/kqdlxxb-2018.0237
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Software development of ultra-scale numerical simulaiton for aero-elastic problem (2017)
WANG Yuntao, MENG Dehong, SUN Yan, HONG Junwo
2018, 36(6): 1019-1026. DOI: 10.7638/kqdlxxb-2018.0030
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Aerodynamic nonlinearity for surface vibration in supersonic flow
LIU Cheng, YE Zhengyin
2018, 36(6): 1027-1033. DOI: 10.7638/kqdlxxb-2018.0057
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Experiments on vortex-induced vibration of a circular cylinder in wind tunnel
LYU Zhen, LIU Fuqun, ZHANG Weiwei, Li Xintao, Diwu Qiangqiang
2018, 36(6): 1034-1040. DOI: 10.7638/kqdlxxb-2018.0048
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Study on whirl-flutter stability of a tiltrotor aircraft
DENG Xudong, HU Heping
2018, 36(6): 1041-1046. DOI: 10.7638/kqdlxxb-2018.0051
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Topology optimization of high-aspect-ratio wing section considering aeroelastic effect
LYU Ji'nan, GUO Li, FAN Xueling, CHEN Gang, LIU Ziqiang
2018, 36(6): 1047-1051. DOI: 10.7638/kqdlxxb-2018.0024
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Gust response analysis for helicopter rotors coupled with fuselage in different flights
WANG Linpeng, DAI Yuting, TANG Changhong
2018, 36(6): 1052-1060. DOI: 10.7638/kqdlxxb-2018.0036
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One way fluid-structure and thermo-structure interaction on an inflatable space re-entry aeroshell
ZHANG Zhang, WU Jie, HOU Anping, WANG Liwu, ZHU Meifang
2018, 36(6): 1061-1070. DOI: 10.7638/kqdlxxb-2018.0033
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