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Vehicle aerodynamic sensing technology based on surface distributed pressure
SUN Rong, LI Linkai, GU Yunsong, LUO Shuai
2025, 39(5): 1-10. DOI: 10.11729/syltlx20230008
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Investigation on error correction method of five-holes probes used in flow field with large velocity gradient
XIE Jinwei, GUO Tao, ZHANG Jing, LIU Cunliang
2025, 39(5): 11-18. DOI: 10.11729/syltlx20230009
Abstract PDF
Development and experimental analysis of circular foil pressure-heat flux gage
ZHU Xinxin, YANG Yuanjian, WANG Hui, LI Zeyu, LUO Yue
2025, 39(5): 19-27. DOI: 10.11729/syltlx20230044
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Research on FADS technology of diamond-nosed aircraft without stagnation pressure
ZHANG Zongyuan, GU Yunsong, LI Linkai, ZHAO Dongkai
2025, 39(5): 28-36. DOI: 10.11729/syltlx20230125
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Roll-yaw control of flying wing aircraft at a high angle of attack based on jet control
GE Zengran, SHI Zhiwei, DONG Yizhang, CHEN Kun, CHEN Jie
2025, 39(5): 37-45. DOI: 10.11729/syltlx20220104
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Preliminary experimental study on the crushing length of centrifugal single and double injectors liquid film
KANG Jinxin, TONG Yiheng, HUANG Kejia, GUO Kangkang, FENG Songjiang
2025, 39(5): 46-52. DOI: 10.11729/syltlx20230084
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Research on anti time-varying disturbance control of wind tunnel flow field
LIU Weijie, LING Zhongwei, DENG Xiaoman, YAN Cheng, CHEN Haifeng, XIAO Jin
2025, 39(5): 53-59. DOI: 10.11729/syltlx20230093
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Experimental study on the effect of rough surface on aerodynamic characteristics and flow field of low Reynolds number airfoil
DENG Haodong, XIA Tianyu, DONG Hao, CHENG Keming
2025, 39(5): 60-72. DOI: 10.11729/syltlx20230032
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Experimental research on surface acoustic load of helicopter fuselage
LIU Shaoteng, LIU Xiangnan, SHAO Tianshuang, DING Cunwei, YU Wenkai
2025, 39(5): 73-79. DOI: 10.11729/syltlx20220106
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Temperature-difference-based heat-flux sensors and their application in hypervelocity low-density wind tunnel
YANG Kai, WANG Hongyu, ZHU Xinxin, ZHU Tao, CHEN Xi, TAO Bowan, LI Jie
2025, 39(5): 80-87. DOI: 10.11729/syltlx20230140
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Mach 6 boundary layer transition experiment on windward side of a HyTRV model
TU Guohua, WANG Ao, LIU Shuyi, HUANG Ganglei, DUAN Maochang, XU Yang, CHEN Jianqiang
2025, 39(5): 88-99. DOI: 10.11729/syltlx20240013
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The experimental investigation of ramjet inlet aeroelasticity
TIAN Haitao, YUAN Kaihua, HE Haibo, HOU Liangxue, CHENG Meng
2025, 39(5): 100-107. DOI: 10.11729/syltlx20230155
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Experimental study on blade tip vortex strength suppression using plasma synthetic jets
ZHANG Tao, CHEN Chen, CAO Yaxiong, ZENG Wei, MENG Yiwei, LIU Rubing, LIN Qi
2025, 39(5): 108-120. DOI: 10.11729/syltlx20230088
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Design of measurement and control system for helicopter carrier landing aerodynamic characteristics experiment
CHE Binghui, ZHAO Guangyin, SHI Zheyu, ZHANG Guichuan, PENG Xianmin
2025, 39(5): 121-127. DOI: 10.11729/syltlx20230007
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Design and application of millisecond rapid-opening valve for high pressure gas-driven light gas gun
ZOU Shengyu, JIAO Dezhi, LONG Renrong, LAN Shengwei
2025, 39(5): 128-137. DOI: 10.11729/syltlx20230091
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