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| Load Conversion of Vibration Fatigue Test Based on Damage Equivalence |
| YIN Xiang-hong, WANG Ke, CHEN Guo-ping, YANG Li-bing |
| 2022,19(9):1-6 |
| Abstract(2370) View PDF(1109) |
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| Analysis of Vibration Response of Aircraft Gun Cabin Structure |
| DING Zhen-hao, WANG Ke, WANG He-zhe |
| 2022,19(9):7-11 |
| Abstract(2524) View PDF(1113) |
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| Vibration Fatigue Life Analysis of Stiffened Plates under Complex Loads |
| XIONG Jia-lin, WANG Ke, ZHOU Su-feng |
| 2022,19(9):12-17 |
| Abstract(2095) View PDF(1018) |
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| Time-dependent Damage Performance Study of Piezoelectric Ceramics for Vibration Control of Flexible Plates |
| QIU Zhi-yong, WANG Ke, LIN Ye, LI Qiang |
| 2022,19(9):18-24 |
| Abstract(2027) View PDF(1030) |
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| Mechanism Configuration and Dynamic Analysis of Bionic Legged Terrain Adaptive Landing Gear |
| LIU Hao-lin, LIU Xiao-chuan, REN Jia, WANG Ji-zhen, YANG Zheng-quan |
| 2022,19(9):25-31 |
| Abstract(2555) View PDF(1080) |
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| Prediction of Broadband Sound Insulation of Stiffened Panels Based on Hybrid FE-SEA Method |
| PENG Tao, HAN Peng-cheng, LIU Xing-qiang, YAN Qun, ZOU Xue-feng, QI Zhi-min |
| 2022,19(9):32-38 |
| Abstract(1930) View PDF(1024) |
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| Simulated Analysis of Impact Damage of Typical ReinforcedComposite Panels by Drop Hammer/Hail |
| HAN Si-cong, HOU Rui, REN Shan, ZHAO Chen, ZHANG Rui-chen |
| 2022,19(9):39-45 |
| Abstract(2800) View PDF(1186) |
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| Dynamic Simulation and Experimental Verification of Carrier-based Aircraft |
| ZHANG Hao-cheng, ZHI Ya-fei, LI Yong-gang, XU Yan |
| 2022,19(9):46-53 |
| Abstract(2562) View PDF(1081) |
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| The Influence of Cabin Door Vibration on Cabin Noise Characteristics |
| HU Chen-ying, GAO Fei |
| 2022,19(9):54-60 |
| Abstract(2205) View PDF(1079) |
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| Dynamic Simulation of Telescopic Mechanism for Morphing Aircraft in the Condition of Heavy Loads and Large Deformations |
| HUANG Hu, WU Xing-wen, ZHANG Fan, HU Li |
| 2022,19(9):61-68 |
| Abstract(2299) View PDF(1048) |
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| Nonlinear Vibration Characteristics of Metal Rubber Vibration Isolator Based on Average Method |
| YIN Yuan-xi, YANG Li, DUAN Yu-xing, ZHAO Jing |
| 2022,19(9):69-77 |
| Abstract(2167) View PDF(1152) |
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| Identification and Modification of Aircraft's Dynamic Characteristics by Control Surfaces' Oscillation Excitation Flight Test |
| ANG Pei-sen |
| 2022,19(9):78-82 |
| Abstract(2086) View PDF(997) |
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| Vibration Absorption Technology on the Support Structure of Main Gearbox for Helicopter Cabin Noise Reduction |
| WANG Feng-jiao, LI Ao, LI Ming-qiang, LI Jian-wei |
| 2022,19(9):83-91 |
| Abstract(2642) View PDF(1108) |
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| Comparative Analysis of Different Failure Modes of Thermoplastic Composites under High Speed Impact |
| DANG Xiao-yan, JI Fei, ZHANG Lei, YANG Wei-ping |
| 2022,19(9):92-102 |
| Abstract(2314) View PDF(1148) |
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| Dynamic Response Analysis of Aircraft Maneuverbased on Aeroelastic Model |
| LIU Ping |
| 2022,19(9):103-107 |
| Abstract(2252) View PDF(993) |
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| Modal Analysis of the Whole Launch Vehicle Based on Three-Dimensional Dynamic Numerical Model and Test Data Reuse Techniques |
| LI Shuang, ZHU Xi-quan, HONG Liang-you, YANG Shu-tao, LIU Liang, LIU Si-hong |
| 2022,19(9):108-113 |
| Abstract(2348) View PDF(1078) |
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| Launch Dynamic Response of an Aircraft Gun with Uncertain Parameters |
| WANG Jing, YANG Yong-feng |
| 2022,19(9):114-122 |
| Abstract(2305) View PDF(1039) |
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| Diagnosis and Treatment Technology of Typical Abnormal Vibration of Fly-by-Wire Aircraft |
| JU Li-feng, QU Xiao-yu, LEI Ming, KOU Bao-zhi |
| 2022,19(9):129-136 |
| Abstract(2595) View PDF(1107) |
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