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Research on mechanism of transonic area rule in near field
Wang Ganglin, Zheng Sui
2016, 30(4): 1-6. DOI: 10.11729/syltlx20160024
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Experimental study on Reynolds number effect on aerodynamic pressure and forces of cylinder
Liu Qingkuan, Shao Qi, Zheng Yunfei, Li Conghui, Ma Wenyong, Liu Xiaobing
2016, 30(4): 7-13. DOI: 10.11729/syltlx20150112
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Experimental study on leak detection of cooling water in arc heater based on emission spectroscopy
Lin Xin, Chen Lianzhong, Dong Yonghui, Ou Dongbin, Li Fei, Yu Xilong
2016, 30(4): 14-19. DOI: 10.11729/syltlx20150155
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Investigation on formation flight in wind tunnel
Liu Zhiyong, Tao Yang, Shi Zhiwei, Geng Xi, Yin Xiezhen
2016, 30(4): 20-25. DOI: 10.11729/syltlx20150099
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Numerical study of ground effects on high speed train aerodynamic drag
Zhou Jian, Ou Ping, Liu Peiqing, Guo Hao
2016, 30(4): 26-31. DOI: 10.11729/syltlx20150124
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The effect of detector installing structure on wall temperature measurement of vehicle
Shi Anhua, Shi Weibo, Sun Haihao, Liu Chunsheng, Han Dong, Huang Jie
2016, 30(4): 32-36. DOI: 10.11729/syltlx20160021
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Experimental and CFD study on the mechanism of supercritical airfoil drag reduction with micro vortex generators
Zhang Jin, Liu Jingyuan, Zhang Binqian
2016, 30(4): 37-41. DOI: 10.11729/syltlx20150157
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Test investigation of the aerodynamic characteristics of grid fins for configuration with body and fins
Song Shuheng, He Cao, Li Yonghong, Zhou Ling, Huang Yong
2016, 30(4): 42-47. DOI: 10.11729/syltlx20140069
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Experimental study on characteristics of the liquid holdup during mobile pipe draining
Jiang Junze, Zhang Weiming, Yong Qiwei, Jiang Ming
2016, 30(4): 48-55. DOI: 10.11729/syltlx20150152
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Implementation and research on the reconstruction algorithms of pressure fields based on PIV
Liu Shun, Xu Jinglei, Yu Kaikai
2016, 30(4): 56-65. DOI: 10.11729/syltlx20150119
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Development and application of the force-measuring balance in impulse combustion wind tunnel tests
He Wei, Gao Chang, Zhang Xiaoqing, Yu Shien
2016, 30(4): 66-70. DOI: 10.11729/syltlx20160011
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Study on model base pressure measuring technique in hypersonic wind tunnel
Xie Fei, Guo Leitao, Zhang Shaowu, Cao Cheng, Zou Qiongfen
2016, 30(4): 71-75. DOI: 10.11729/syltlx20150043
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Study and development of total pressure probe and pitot tube in 3m×2m icing wind tunnel
Zu Xiaoyong, Zhang Lin, Xiao Bin, Zhu Shimin
2016, 30(4): 76-80. DOI: 10.11729/syltlx20160006
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Research on key technologies of debugging and operating in 0.6m×0.6m continuous transonic wind tunnel
Xiong Bo, Zhou Enmin, Cheng Song, Zhang Wen, Liu Kai, Luo Xinfu
2016, 30(4): 81-86. DOI: 10.11729/syltlx20150052
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The design of total pressure control strategy for 0.6m continuous transonic wind tunnel
Li Zhuangsheng, Yang Pengcheng, Chen Dan, Zhang Yongshuang, Guo Shouchun, Chen Tianyi
2016, 30(4): 87-92. DOI: 10.11729/syltlx20150129
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Investigation on the flow rotation effect and elimination in hypersonic wind tunnel
Chen Aiguo, Li Xuguo, Mao Chunman, Sun Liangbao, Long Yongsheng, Yang Yanguang
2016, 30(4): 93-96. DOI: 10.11729/syltlx20150146
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Design of nozzle inviscid contour based on axial Mach number distribution
Hu Zhenzhen, Li Zhenqian, Shi Yilei, Chen Aiguo
2016, 30(4): 97-104. DOI: 10.11729/syltlx20150115
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