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2023(12): 1-8.
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2023, 41(12): 1-4.
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2023, 41(12): 1-1.
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A constrained slip-wall boundary condition based on discrete equivalent equations
WEI Yanxin, LIU Jun
2023, 41(12): 1-15. DOI: 10.7638/kqdlxxb-2023.0018
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Optimization design on the wing of a general aviation airplane based on deep belief network and multi-objective particle swarm optimization algorithm
WU Yongchuan, SUN Gang, TAO Jun
2023, 41(12): 16-27. DOI: 10.7638/kqdlxxb-2023.0005
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Study on the convergence criterion of linear iteration in inexact Newton methods
FENG Xuanyan, YAN Zhenguo, ZHU Huajun, MA Yankai, FENG Xinlong
2023, 41(12): 28-36. DOI: 10.7638/kqdlxxb-2023.0001
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Numerical study on compressible gas-solid two-phase flow based on a particle solver implemented in NNW-PHengLEI
LEI Yinghaonan, LEI Sanhui, ZHANG Shenghao, WANG Ping
2023, 41(12): 37-47. DOI: 10.7638/kqdlxxb-2022.0161
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Vorticity transport characteristics of separated shear layer under AC/NS-DBD plasma actuation
ZHAO Guangyin, YANG Yongdong, LI Tingting, XIAO Chunhua, YAN Li
2023, 41(12): 48-60. DOI: 10.7638/kqdlxxb-2022.0163
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Influence of the number of blades on aerodynamic and noise characteristics of counter-rotating propeller
CUI Panwang, FENG Heying, TONG Fan, CHEN Zhengwu
2023, 41(12): 61-73. DOI: 10.7638/kqdlxxb-2022.0205
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Experiment of the effect of propeller slipstream on single-engine airplanes
LIU Wei, ZHAO Zhong, ZHANG Shouyou, XIE Lu
2023, 41(12): 74-81. DOI: 10.7638/kqdlxxb-2022.0197
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2023, 41(12): 82-82.
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Research status and development tendency of large aircraft wind tunnel technologies in China
WU Junqiang, CUI Xiaochun, WEI Zhi, DU Wentian
2023, 41(12): 83-94. DOI: 10.7638/kqdlxxb-2023.0147
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Test techniques and data correction method for large airplanes in a 2.4 m intermittent transonic wind tunnel
XU Xin, LI Qiang, PENG Xin, JIANG Hong, LIU Dawei, WU Junqiang
2023, 41(12): 95-106. DOI: 10.7638/kqdlxxb-2023.0137
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Integrated application of PIV and PSP in large aircraft wind tunnel test
SHANG Jinkui, LI Yujun, ZHAO Ronghuan, WANG Meng, ZHONG Hongjie, XU Zhaonan, CUI Xiaochun
2023, 41(12): 107-117. DOI: 10.7638/kqdlxxb-2023.0152
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Precision force measurement techniques for large aircraft models in 2.4 m continuous transonic wind tunnel
ZHANG Ren, XU Zhifu, LI Xiaogang, LIU Yu, ZHANG Ying, DU Wentian
2023, 41(12): 118-132. DOI: 10.7638/kqdlxxb-2023.0167
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2023, 41(12): 133-133. DOI: 10.7638/kqdlxxb-2023.202312bwmd
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