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Experimental studies of Curved Cone Waverider forebody Inlet(CCWI) at low Mach number range
Wei Feng, Zhou Zheng, Li Li, He Xuzhao
2017, 31(6): 1-7. DOI: 10.11729/syltlx20170049
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Investigation of turbulence modification by PIV tracer particles in a supersonic mixing layer
Chen Xiaohu, Chen Fang, Liu Hong, Sha Sha, Lu Xueling, Zhang Qingbing
2017, 31(6): 8-14, 21. DOI: 10.11729/syltlx20160144
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PIV measurement on streamwise vortex generated by undulating fins
Zhang Jun, Bai Yaqiang, Zhai Shucheng, Zhang Guoping, Xu Lianghao
2017, 31(6): 15-21. DOI: 10.11729/syltlx20170017
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Experimental investigation on the effects of vortex generator on corner separation in a high-load compressor cascade
Li Renkang, Wang Rugen, He Cheng, Hu Jiaguo, Ma Caidong, Huang Danqing
2017, 31(6): 22-28, 36. DOI: 10.11729/syltlx20160195
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Experimental study of coherent structures in a solid-liquid turbulent boundary layer
Zhao Huiling, Sun Jiao, Xuan Ruixiang, Chen Wenyi
2017, 31(6): 29-36. DOI: 10.11729/syltlx20160199
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Hypersonic wind tunnel flutter test research on rudder models by continuously varying dynamic pressure
Ji Chen, Zhao Ling, Zhu Jian, Liu Ziqiang, Li Feng
2017, 31(6): 37-44. DOI: 10.11729/syltlx20170088
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Wind tunnel drop model test of nose cap separation of supersonic vehicle
Song Wei, Lu Wei, Jiang Zenghui
2017, 31(6): 45-50, 70. DOI: 10.11729/syltlx20170026
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Research on application of Rayleigh scattering velocity measurement in hypersonic low density wind tunnel
Chen Aiguo, Chen Li, Li Zhihui, Li Zhonghua, Yang Furong, Li Sixin, Yan Bo
2017, 31(6): 51-55. DOI: 10.11729/syltlx20170020
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Research of the measurement method for the pressure distribution along the micro/mini-channel
Wang Haoli, Wang Bing
2017, 31(6): 56-61. DOI: 10.11729/syltlx20170050
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Application of additive manufacturing to 30CrMnSiA high speed wind tunnel test model design and fluid-structure interaction analysis
Hong Xingfu, Ye Cheng, Wang Linzhi
2017, 31(6): 62-70. DOI: 10.11729/syltlx20170074
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Research on metric thrust jet-effects testing methodology in high-speed wind tunnel
Ji Jun, Song Xiaoyu, Deng Xiangdong, Guo Dapeng, Li Peng
2017, 31(6): 71-77. DOI: 10.11729/syltlx20160176
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Development and application of the measurement system for thrust vectoring tests at 2.4m×2.4m transonic wind tunnel
Miao Lei, Xie Bin, Li Jianqiang, Li Yaohua, Huang Cundong, Jia Wei, Ma Tao
2017, 31(6): 78-85. DOI: 10.11729/syltlx20160105
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Investigation on test technique for hypersonic flow-through model nozzle outlet airflow parameters measurement
Shu Haifeng, He Chao, Guo Leitao, Xu Xiaobin, Fan Xiaohua
2017, 31(6): 86-92, 99. DOI: 10.11729/syltlx20160018
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Research on control method of spraying system in the icing wind tunnel
Li Shucheng, Luo Qiang, Chen Dan, Huang Weikai
2017, 31(6): 93-99. DOI: 10.11729/syltlx20160036
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Design and application of wind tunnel strain gauge balance protective device based on 3D printing
Xiang Guangwei, Wang Chao, Wan Liqiang, Mi Peng, Wang Shumin
2017, 31(6): 100-104. DOI: 10.11729/syltlx20160114
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