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An overview of supercooled large droplets icing condition simulation capability in icing wind tunnels
Fu Cheng, Song Wenping, Peng Qiang, Liao Daxiong, Wang Chao
2017, 31(4): 1-7. DOI: 10.11729/syltlx20160118
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Advances influidic thrust vectoring technique research
Xiao Zhongyun, Jiang Xiong, Mou Bin, Chen Zuobin
2017, 31(4): 8-15. DOI: 10.11729/syltlx20160207
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Measuring DLVO force and surface potential based on AFM colloidal probe technique at liquid-solid interfaces
Tian Weifang, Zheng Xu, Li Zhanhua, Xu Zheng
2017, 31(4): 16-21. DOI: 10.11729/syltlx20160163
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Experiment study of propulsion-induced flow on aircraft aerodynamics
Zhang Chao, Zhu Jihong, Wu Linfeng, Li Huanyu, Li Chunwen
2017, 31(4): 22-27, 33. DOI: 10.11729/syltlx20160154
Abstract PDF
Laser absorption spectroscopy diagnostics in the arc-heater of an arcjet facility
Zeng Hui, Chen Lianzhong, Lin Xin, Ou Dongbin, Dong Yonghui
2017, 31(4): 28-33. DOI: 10.11729/syltlx20160179
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Design of civil aircraft's static source aerodynamic layout
Yang Hui, Yang Shipu, Huang Di, Sun Yifeng
2017, 31(4): 34-38, 58. DOI: 10.11729/syltlx20160109
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Blade tip vortex measurements of a hovering rotor
Liu Ping'an, Lin Yongfeng, Chen Yaofeng, Yuan Mingchuan
2017, 31(4): 39-44. DOI: 10.11729/syltlx20160186
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The seawater surface tension coefficient representation with different salinities
Zhang Zhiyou, Jin Liang'an, Yuan Zhijiang, He Shengyang
2017, 31(4): 45-50. DOI: 10.11729/syltlx20160164
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A dynamic calibration method for a dynamometric system in impulse combustion facilities
Wu Long, Wang Feng, Le Jialing
2017, 31(4): 51-58. DOI: 10.11729/syltlx20160158
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Study on technology of using flaky hinge moment balance for high-aspect-ratio wings based on external electric bridge correction method
Jia Wei, Liu Weiliang, Zhao Zhongliang, Miao Lei, Xie Bin, Mi Peng, Yang Hongsheng, Wang Shumin, Chen Zhu
2017, 31(4): 59-63. DOI: 10.11729/syltlx20160107
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General data processing system for multiple wind tunnels
Deng Xiaoman, Fan Jinlei, Yu Li, Li Chunyan, He Fu
2017, 31(4): 64-70. DOI: 10.11729/syltlx20170051
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Thermodynamics model updating of cryogenic wind tunnel diffuser based on response surface method
Ma Yueyin, Nie Xutao, Chen Wanhua, Yao Chengwei, Zhang Wei
2017, 31(4): 71-78. DOI: 10.11729/syltlx20160133
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Experimental investigation on critical pressure ratio of hypersonic wind tunnel vacuum system
Chen Aiguo, Li Zhenqian, Qi Dawei, Long Zhengyi, Yang Yanguang
2017, 31(4): 79-83, 96. DOI: 10.11729/syltlx20160115
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Research on method for evaluating the thermal protective performance of non-catalysis material in non-equilibrium flow
Yu Mingxing, Bai Shuxin, Xu Xiaoliang, Cao Zhanwei
2017, 31(4): 84-89. DOI: 10.11729/syltlx20170084
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Uncertainty assessment for aerodynamic test in Φ0.5m hypersonic wind tunnel
Liu Chunfeng, Xiong Lin
2017, 31(4): 90-96. DOI: 10.11729/syltlx20160121
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