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Display Method:
Progress in rough-wall turbulence
WANG Jianjie, YI Haiming, PAN Chong, WANG Jinjun, LI Tian
2017, 35(5): 611-619. DOI: 10.7638/kqdlxxb-2017.0033
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Development and precision validation of static aeroelastic computational module on flow solver TRIP
SUN Yan, HUANG Yong, WANG Yuntao, MENG Dehong, WANG Hao
2017, 35(5): 620-624. DOI: 10.7638/kqdlxxb-2015.0154
Abstract PDF
An aerodynamic analysis tool for aircraft conceptual design at full speed range
LYU Fanxi, LI Zhengzhou, DENG Jingshu, XIAO Tianhang, YU Xiongqing
2017, 35(5): 625-632. DOI: 10.7638/kqdlxxb-2016.0152
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Investigation on design of Φ240mm hypersonic wind tunnel diffuser
FAN Xiaohua, YANG Bo, ZHU Tao, ZHONG Jun
2017, 35(5): 633-639. DOI: 10.7638/kqdlxxb-2015.0077
Abstract PDF
Computational method on hypersonic aerodynamic heating for aerospace vehicle
WANG Peng, FANG Shuai, JIN Xin, ZHANG Weimin
2017, 35(5): 640-644. DOI: 10.7638/kqdlxxb-2015.0067
Abstract PDF
Effect of chamfer rear-face angle on open cavity flow aero-acoustic noise suppression
WU Jifei, XU Laiwu, FAN Zhaolin, LUO Xinfu
2017, 35(5): 645-649. DOI: 10.7638/kqdlxxb-2015.0047
Abstract PDF
Flow field simulation for a helicopter rotor in transient flying with ground effect
XIN Ji, MA Chengjiang, LI Pan, CHEN Renliang
2017, 35(5): 650-654. DOI: 10.7638/kqdlxxb-2015.0066
Abstract PDF
Numerical study on aerodynamic characteristics of wing-in-ground and effect of end plates
YU Haichuan, LI Dun, HE Yuelong, LIU Shuai
2017, 35(5): 655-658. DOI: 10.7638/kqdlxxb-2015.0198
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Dynamic response of the wind turbine blade bending in the rotational plane
LI Yijin, WANG Tongguang, QIAN Yaoru
2017, 35(5): 659-664. DOI: 10.7638/kqdlxxb-2016.0119
Abstract PDF
Some phenomena of vortex-induced vibration in super high-rise building
WANG Lei, ZHANG Zhenhua, LIANG Shuguo, WANG Shuliang, ZOU Lianghao
2017, 35(5): 665-669. DOI: 10.7638/kqdlxxb-2015.0184
Abstract PDF
Demonstration and validation flight test of scaled aircraft model and its key technologies
HE Kaifeng, MAO Zhongjun, WANG Qing, CHEN Hai
2017, 35(5): 671-679. DOI: 10.7638/kqdlxxb-2017.0089
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High-speed wind tunnel free-flight test technique
JIANG Zenghui, SONG Wei, LU Wei
2017, 35(5): 680-686, 692. DOI: 10.7638/kqdlxxb-2016.0101
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Wind tunnel free-flight test for stage separation of tandem layout vehicle
SONG Wei, JIANG Zenghui
2017, 35(5): 687-692. DOI: 10.7638/kqdlxxb-2016.0077
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Similarity criteria and simulation method for flight control system of free-flight test in low speed wind tunnel
LIU Zhitao, CEN Fei, NIE Bowen, FAN Litao, SUN Haisheng
2017, 35(5): 693-699. DOI: 10.7638/kqdlxxb-2017.0029
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Rapid prototyping and implementation of flight control system for wind tunnel virtual flight test
LIU Zhitao, NIE Bowen, GUO Linliang, ZHU Minghong
2017, 35(5): 700-707. DOI: 10.7638/kqdlxxb-2017.0026
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Modeling and simulation for a low speed wind tunnel virtual flight test rig
GUO Linliang, ZHU Minghong, FU Hao, KONG Peng, ZHONG Chengwen
2017, 35(5): 708-717, 726. DOI: 10.7638/kqdlxxb-2017.0164
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An improved dynamic surface control law and its application in post-stall maneuvers
ZHANG Sheng, WANG Qing, HE Kaifeng, SHAO Yuanpei
2017, 35(5): 718-726. DOI: 10.7638/kqdlxxb-2017.0092
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A new high speed model flight test scheme carried by helium balloon
SHAO Yuanpei, CHENG Yanqing, HE Kaifeng, YU Yonggang, ZHOU Yu
2017, 35(5): 727-731, 741. DOI: 10.7638/kqdlxxb-2017.0122
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Surface pressure and temperature measurement technology in MF-1 modelling flight test
YANG Qingtao, ZHOU Yu, YUAN Xianxu, GUAN Rui, QIU Jinhao
2017, 35(5): 732-741. DOI: 10.7638/kqdlxxb-2017.0167
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Key problems in structure and thermal protection for MF-1 model testing flight vehicle
OU Chao, JI Hongliang, XIAO Hanshan, YUAN Xianxu, WANG Anling
2017, 35(5): 742-749. DOI: 10.7638/kqdlxxb-2017.0170
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