[1] |
FENG Zhenyu, LIU Xu, LIN Lanhui, YANG Yongpan, XIE Jiang, SHI Xiaopeng, XIAO Pei, LI Leizi, YI Pengfei, LIU Xiaochuan, BAI Chunyu.
Impact of seatbelts on impact characteristics of aviation seats and occupants
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 224808-224808.
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[2] |
LI Hongwei, CHEN Qinggui, XU Xiaoli, HONG Jie.
Reliability analysis of same stage blade system with common failure dependence
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(7): 222803-222803.
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[3] |
CHAI Guozhong, LYU Jun, BAO Yumei, JIANG Xianfeng, DING Hao.
A highly efficient and accurate numerical analysis method for fatigue propagation of surface crack and life prediction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(12): 221291-221291.
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[4] |
LI Hongrui, XU Xiaoxiao, LIU Chao, LIU Xinxin.
Flow direction effect on heat transfer of supercritical CO2 in helically coiled tube
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(7): 2123-2131.
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[5] |
HONG Zhiliang, GAO Ge, JING Xiaodong, SUN Xiaofeng.
A grid-less time domain method for plate trailing edge noise prediction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(11): 3501-3514.
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[6] |
PENG Changxin, WANG Zhiwu, ZHENG Longxi.
Numerical Investigation of Effect of Detonation Chamber Length on Back-propagation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(5): 1001-1008.
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[7] |
ZHOU Junhui, ZHANG Jingzhou.
Numerical Investigation on Particle Deposition Characteristic Inside Turbine Cascade
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(11): 2492-2499.
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[8] |
GU Xingjin, XU Xiwu.
Numerical Simulation of Damage in Stiffened Integral Composite Panels Under High Velocity Impact
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(2): 258-272.
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[9] |
YU Chong, WANG Xu, CHEN Peng, SU Xinbing.
Study of Control Characteristics for All Moving Wing Tips in Delta Wing Tailless Configuration
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(11): 1975-1983.
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[10] |
ZHANG Lishuang, WANG Tongqing, YANG Bing, ZHANG Wei.
Numerical Simulation of Sound Propagation from Varying Cross-section Ducts by Fast Scattering Method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(1): 62-67.
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[11] |
NAN Xiangjun, ZHANG Kunyuan, JIN Zhiguang, SUN Bo.
Numerical and Experimental Investigation of Hypersonic Inward Turning Inlets with Rectangular to Circular Shape Transition
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(6): 988-996.
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[12] |
Wang Xiaowei;Jin Ping;Cai Guobiao.
Scaling of Gas-gas Cold Flow Fields
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(7): 1305-1311.
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[13] |
Yang Maosheng;Chen Yueliang.
Finite Element Analysis of Stress Intensity Factors of Fretting Fatigue Structure
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(10): 1968-1973.
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[14] |
DU Lin;WANG Xiao-yu;SUN Xiao-feng.
A New Approach for the Acoustic Design of Aeroengine Nacelle
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(6): 1068-1072.
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[15] |
WANG Xiao-yu;DU Lin;SUN Xiao-feng.
A New Approach for the Acoustic Design of Aeroengine Nacelle with the Effect of Varying Cross-section Aera
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(6): 1073-1079.
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