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The experimental investigation on the effect of rearward Mini-TED to the aerodynamic characteristics of an airfoil
Xia Jun, Daichin
2015(5): 1-7,25. DOI: 10.11729/syltlx20140148
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Research on aerodynamic parameter identification technology in wind tunnel free-flight test based on Maximum Likelihood Estimation
Zhang Tianjiao, Qian Weiqi, He Kaifeng, Wang Qing
2015(5): 8-14. DOI: 10.11729/syltlx20140116
Abstract PDF
Study on error mechanism and uncertainty assessment of heat flux measurement in shock tunnel
Zeng Lei, Gui Yewei, Wang Anling, Qin Feng, Zhang Haoyuan
2015(5): 15-25. DOI: 10.11729/syltlx20140135
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Experimental study of turbulent mixing of the cloud with unsaturated air under different humidity
Liu Xiaoxia, Lu Zhiming, Huang Yongxiang, Zhou Quan, Liu Yulu
2015(5): 26-31,44. DOI: 10.11729/syltlx20150017
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Optimization design of inner-structure of the slot-jet in aircraft cabin based on investigation of multi-scale characteristics of slot turbulent jet flow
Ge Wentao, Guo Yong, Dai Shen, Jiang Nan, Liu Junjie
2015(5): 32-37. DOI: 10.11729/syltlx20140151
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Design and experimental analysis of three-stage compression cone-derived waverider
Lyu Zhenjun, Wang Xudong, Ji Weidong, Wang Jiangfeng
2015(5): 38-44. DOI: 10.11729/syltlx20150003
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Research on optimal design method for wind tunnel strain gauge balance based on iSIGHT
Xiang Guangwei, Wang Jie, Shi Yujie, Yi Guoqing
2015(5): 45-49,59. DOI: 10.11729/syltlx20150013
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Strain gauge balance development for force test on small aspect ratio flying wing high speed standard model
Shi Yujie, Huang Yong, Tian Zhengbo
2015(5): 50-54. DOI: 10.11729/syltlx20150015
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Research on the wind tunnel test techniques for micro-pitching-aerodynamics of re-entry body
Zhao Junbo, Fu Zengliang, Liang Bin, Zhang Shiyu, Gao Qing
2015(5): 55-59. DOI: 10.11729/syltlx20150027
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Measurements of cylinder’s wake by Tomo-PIV
Xu Xianghui, Jiang Jiali, Niu Zhongguo, Ning Jipeng, Liu Jie
2015(5): 60-64. DOI: 10.11729/syltlx20150022
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Uncertainty analysis in submarine standard model resistance test
Shi Shengzhe, Zheng Yaxiong
2015(5): 65-71. DOI: 10.11729/syltlx20150002
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Research on flutter test technology of continuously adjusting dynamical pressure in high-speed wind tunnel
Guo Hongtao, Yan Yu, Yu Li, Lyu Binbin, Du Ning
2015(5): 72-77. DOI: 10.11729/syltlx20150061
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Investigation of aeroacoustic localization technique in lining test section
Chen Bao, Li Zhoufu, Tan Xiao, Li Yuanshou, Shao Tianshuang, Zhang Xue, Jiang Tao
2015(5): 78-83. DOI: 10.11729/syltlx20150035
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Application of PID based on adaptive genetic algorithms in wind velocity control system of wind tunnels
Ni Wenbin, Dong Jingang, Liu Shuwei, He Lihui, Fu Zengliang
2015(5): 84-89. DOI: 10.11729/syltlx20150016
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Ground experimental method for stratospheric propeller plasma flow control
Chen Qingya, Tian Xihui, Che Xueke, Nie Wansheng, Zhou Siyin
2015(5): 90-96. DOI: 10.11729/syltlx20140140
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