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2023, 41(1)
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The capability of aerodynamic ground test in the USA and its development trend analysis
SUN Zongxiang, LI Wenjia, TANG Zhigong, GUO Chuwei, LUO Yuepei, SUN Hangyi
2023, 41(1): 1-21. DOI: 10.7638/kqdlxxb-2022.0179
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Aerodynamic design of 2.4 m continuous transonic wind tunnel
ZHANG Ren, DU Wentian, LI Qingli, CUI Xiaochun
2023, 41(1): 22-38. DOI: 10.7638/kqdlxxb-2022.0185
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Design and preliminary freestream calibration of HUST Φ 0.5 m Mach 6 Ludwieg tube wind tunnel
HUANG Ranran, ZHANG Chengjian, LI Chuangchuang, XU Binghui, XU Duolong, YUAN Xianxu, WU Jie
2023, 41(1): 39-48, 85. DOI: 10.7638/kqdlxxb-2022.0146
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Progress and application of large-flux high-pressure gas reducing valve
XU Wanwu, YE Wei, LI Zhiyan, ZHANG Zhenkang, ZHANG Fuqiang
2023, 41(1): 49-56. DOI: 10.7638/kqdlxxb-2022.0173
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New progress of 3 m × 2 m icing wind tunnel test technology from 2020 to 2022
LIU Senyun, WANG Qiao, YI Xian, ZHANG Pingtao, ZUO Chenglin, GUO Qiling
2023, 41(1): 57-65. DOI: 10.7638/kqdlxxb-2022.0167
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Application of 5.5 m × 4 m aeroacoustic wind tunnel in Sino-Russia joint research collaboration on landing gear noise and its control
ZHAO Kun, WANG Xunnian, SONG Yubao, FAN Zhenglei, KOPIEV Victor
2023, 41(1): 66-76. DOI: 10.7638/kqdlxxb-2022.0152
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Effect of Gurney flaps on aerodynamic characteristics of a spinning missile
KOU Shaobo, FENG Lihao, LI Xiao, YANG Xin, LIU Songbin, XU Huasong
2023, 41(1): 77-85. DOI: 10.7638/kqdlxxb-2021.0401
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Optimal flight test design method based on discrete optimization
LIU Siyu, LIANG Yan, MA Mingming
2023, 41(1): 86-92. DOI: 10.7638/kqdlxxb-2021.0347
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Acoustic modal analysis and pressure transducer array measurements of flow induced acoustic resonances in tandem deep cavities
ZHANG Zhengfan, WANG Peng, WANG Weizhe, LIU Yingzheng
2023, 41(1): 93-100. DOI: 10.7638/kqdlxxb-2021.0275
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Experiments on vortex-induced vibration of a cylinder at subcritical Reynolds numbers
LYU Zhen, ZHANG Weiwei, KOU Jiaqing
2023, 41(1): 101-107. DOI: 10.7638/kqdlxxb-2021.0395
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