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Display Method:
Progress in aeroacoustic investigation of modern large aircraft landing gear
LIU Peiqing, XING Yu, LI Ling, GUO Hao
2017, 35(6): 751-759. DOI: 10.7638/kqdlxxb-2017.0063
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Fast aeroheating prediction method for complex shape vehicles based on proper orthogonal decomposition
NIE Chunsheng, HUANG Jiandong, WANG Xun, LI Yu
2017, 35(6): 760-765. DOI: 10.7638/kqdlxxb-2015.0157
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Contraction design for axis-symmetric nozzles in hypersonic wind tunnel
HU Zhenzhen, LI Zhenqian, CHEN Aiguo, SHI Yilei
2017, 35(6): 766-771. DOI: 10.7638/kqdlxxb-2015.0141
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Assessment of inflow boundary conditions for hypersonic wall bounded turbulent flows
YU Min, YUAN Xiangjiang, ZHU Zhibin
2017, 35(6): 772-776. DOI: 10.7638/kqdlxxb-2015.0177
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Neural network algorithm for FADS system applied to the vehicles with sharp wedged fore-bodies
WANG Peng, HU Yuansi, JIN Xin, ZHANG Weimin
2017, 35(6): 777-780, 791. DOI: 10.7638/kqdlxxb-2015.0064
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Aerodynamic influence of nacelle position of a wing-mounted civil aircraft
ZHANG Dongyun, ZHANG Meihong, WANG Meili, XIANG Chuantao
2017, 35(6): 781-786. DOI: 10.7638/kqdlxxb-2015.0069
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Aerodynamic characteristics analysis for HX analog lifting body
LIU Shenshen, XIE Jing, FENG Yi, TANG Wei, GUI Yewei
2017, 35(6): 787-791. DOI: 10.7638/kqdlxxb-2015.0187
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Lift enhancement control method of thin flat-plate at post stall angles of attack
WU Jifei, WANG Zhijin, GURSUL Ismet
2017, 35(6): 792-796. DOI: 10.7638/kqdlxxb-2015.0068
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Parellel FVTD computation for electromagnetic scattering of electrically large objects
XU Yong, HUANG Yong, YU Yonggang
2017, 35(6): 797-800. DOI: 10.7638/kqdlxxb-2015.0071
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Study on typhoon characteristics at high urban landform altitude and turbulence integral length scale
WANG Chequan, LI Zhengnong, HU Jiaxing, ZHANG Xuewen, ZHOU Lifen, CAO Shoukun
2017, 35(6): 801-806, 822. DOI: 10.7638/kqdlxxb-2015.0090
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Automatic remeshing technique for structured grid based on grid framework
PANG Yufei, LU Fengshun, CAI Yunlong, ZHANG Shujun, SUN Junfeng
2017, 35(6): 807-811. DOI: 10.7638/kqdlxxb-2015.0179
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Method of estimating extreme wind pressure based on the Pareto distribution
LI Zhengnong, CAO Shoukun, Wang Chequan
2017, 35(6): 812-816. DOI: 10.7638/kqdlxxb-2015.0143
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Applications of fluorescence-oil-flow visualization technique in hypersonic wind tunnel test
CHEN Lei, ZHU Tao, XU Yun, JIANG Tao
2017, 35(6): 817-822. DOI: 10.7638/kqdlxxb-2015.0150
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Static port orientation rule for civil aircraft
ZHOU Feng, ZHAO Keliang, ZHANG Miao, WANG Junhong
2017, 35(6): 823-827. DOI: 10.7638/kqdlxxb-2015.0140
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Seal complementation test for rotatable parts in arc heated wind tunnel
YANG Yuanjian, CHEN Dejiang, ZHAO Wenfeng, ZHANG Songhe, JIANG Bo
2017, 35(6): 828-831. DOI: 10.7638/kqdlxxb-2015.0147
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Aerodynamic design of a flying-wing aircraft
YU Yonggang, HUANG Yong, ZHOU Zhu, HUANG Jiangtao
2017, 35(6): 832-836. DOI: 10.7638/kqdlxxb-2015.0163
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Numerical investigation on coupling effects of multiple spouts and lateral jet interaction over missile configuration
JIA Hongyin, WU Xiaojun, ZHOU Naichun, ZHAO Hui
2017, 35(6): 837-840. DOI: 10.7638/kqdlxxb-2015.0083
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Wind tunnel test on transonic static areoelasticity of high-aspect-ratio wing
GUO Hongtao, CHEN Dehua, LYU Binbin, YU Li, ZU Xiaoyong
2017, 35(6): 841-845. DOI: 10.7638/kqdlxxb-2015.0075
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Aerodynamic design and analysis of tip devices on carrier-based fly-wing UAV with stealth constraints
LI Jiguan, CHEN Xin, LI Zhen
2017, 35(6): 846-849. DOI: 10.7638/kqdlxxb-2015.0061
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Gap influence on rudder efficiency of flying wing aircraft
YAO Junkai, CAO Deyi, HE Haibo
2017, 35(6): 850-854. DOI: 10.7638/kqdlxxb-2015.0088
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Study and application of movable icing wind tunnel test method
LI Si, YU Lei, JIN Sha, PEI Runan
2017, 35(6): 855-859. DOI: 10.7638/kqdlxxb-2015.0121
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Numerical damping of dynamic mesh for aerodynamic analysis
ZHAO Zhangfeng, DENG Hongzhou
2017, 35(6): 860-865. DOI: 10.7638/kqdlxxb-2015.0080
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Numerical simulation on cooling characteristics of plate film from backward-expanding shoulder arm hole
HUANG Kang, MA Husheng
2017, 35(6): 866-869. DOI: 10.7638/kqdlxxb-2015.0081
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Ventral support interference in low-speed and high Reynolds number wind tunnel
ZHENG Xinjun, JIAO Renshan, SU Wenhua, MA Honglei, ZHANG Lianhe
2017, 35(6): 870-874. DOI: 10.7638/kqdlxxb-2015.0114
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Inlet and jet test techniques for large scale model in 8m×6m Low Speed Wind Tunnel
CHEN Hong, LIU Litao, WU Chaojun
2017, 35(6): 875-878. DOI: 10.7638/kqdlxxb-2015.0133
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Optimization design for aerodynamic performance of fan-wing aircraft
LI Renfeng, LE Guigao, MA Dawei, CHEN Shuai
2017, 35(6): 879-882, 892. DOI: 10.7638/kqdlxxb-2015.0173
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Flight characteristics of deflected nose projectile
ZHANG Zhiyong, CHEN Zhihua, HUANG Zhengui
2017, 35(6): 883-886. DOI: 10.7638/kqdlxxb-2015.0182
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Sleeve-type afterbody jet experiment technique and its drag correction method
DENG Xiangdong, GUO Dapeng, JI Jun, BAI Yuping, YANG Qinghua
2017, 35(6): 887-892. DOI: 10.7638/kqdlxxb-2015.0113
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Numerical simulation of transonic flow field over delta wing with adaptive overlapped grid system
WANG Na, YE Liang
2017, 35(6): 893-896. DOI: 10.7638/kqdlxxb-2016.0138
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Analysis of wake flow characteristics for low subsonic rocket sled
FANG Ming, SUN Jianhong, WANG Conglei, YU Yuanyuan, Zhang Yantai
2017, 35(6): 897-901. DOI: 10.7638/kqdlxxb-2017.0132
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