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| Application of ABAQUS Secondary Development Based on Python in Modeling of Impact on Composite Laminates |
| CHEN Fang-yu, LI Jin, QIU Wei-zhen, LYU Quan-jiang |
| 2020,17(9):1-6 |
| Abstract(4848) View PDF(3489) |
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| Vibration Response Prediction Based on Helicopter Coupling Analysis |
| FENG Zhi-zhuang, DAI Zhi-xiong, LIU Chen |
| 2020,17(9):7-14 |
| Abstract(4373) View PDF(3455) |
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| Dynamics Simulation Analysis of Carrier Aircraft Landing Arresting Based on PAM-CRASH |
| DANG Xiao-yan, HUANG Chao-guang, FENG Zhen-zhou |
| 2020,17(9):15-20 |
| Abstract(4374) View PDF(3501) |
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| Time Domain Equivalence Simulation Method in Continuous Gust Frequency Response Process |
| LIU Ying-ying, LIU Jing-guang |
| 2020,17(9):21-25 |
| Abstract(4256) View PDF(3473) |
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| Research on Bird Strike Resistance of Empennage Using Aramid Fiber |
| DUAN Li-hui, HUANG Chao-guang, YANG Wei-ping |
| 2020,17(9):26-30 |
| Abstract(4391) View PDF(3523) |
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| Calculation and Experimental Analysis on Different Tail Leading Edge Configurations of Aircraft against Bird Impact |
| DANG Xiao-yan, FENG Zhen-zhou, HUANG Chao-guang |
| 2020,17(9):31-37 |
| Abstract(4336) View PDF(3513) |
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| Calculation and Analysis of Near Field Eddy Current Damping of Permanent Magnet |
| GUO Tong, LI Bin, ZHANG Sheng-kun |
| 2020,17(9):38-42 |
| Abstract(4223) View PDF(3448) |
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| Vibration Responses of the Cockpit Caused by Aerodynamic Sources |
| XIE Wei-jie, YANG Hong-jie |
| 2020,17(9):43-47 |
| Abstract(4277) View PDF(3506) |
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| Simulation Method of Control Surface Impulse Response of Aircraft Flutter Flight Test |
| LEI Ming, LU Xiao-dong, HUO Xing-li |
| 2020,17(9):48-53 |
| Abstract(4593) View PDF(3509) |
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| Analysis Method and Test Technique of Rotor-blade-casing Rub-impact |
| MU Qin-qin, XU Jian, YAN Qun, HUANG Wen-chao |
| 2020,17(9):54-60 |
| Abstract(4478) View PDF(3538) |
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| Theoretical Research for Predicting Crest Factor of Random Vibration Response |
| ZHANG Yu-jie, HUANG Chao-guang, DUAN Li-hui |
| 2020,17(9):61-65 |
| Abstract(4973) View PDF(3520) |
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| Optimization Method for Aircraft Typical Hydraulic Pipeline System¢sVibration Suppression |
| HUANG Hu, MIN Qiang, ZHANG Bao-qiang, WANG Yong-yan |
| 2020,17(9):66-71 |
| Abstract(4511) View PDF(3642) |
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| Design and Test Analysis of Fluidlastic Isolator |
| QIAN Feng, CHENG Qi-you, DAI Zhi-xiong |
| 2020,17(9):72-76 |
| Abstract(4242) View PDF(3407) |
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| Configuration Selection for Design of Bird-strike Resistance of Wing Leading Edge |
| LU Li-jin, FENG Zhen-zhou |
| 2020,17(9):77-82 |
| Abstract(4851) View PDF(3511) |
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| Stochastic Resonance in Fractional-order Underdamped Bistable Systems by Statistical Complexity Measures |
| DANG Pu-ni, SUN Zhong-kui, LYU Jin-feng |
| 2020,17(9):83-88 |
| Abstract(4894) View PDF(3531) |
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| Vibration Control Technology of Thin-wall Structure with Piezoelectric Patches Array |
| LI Kai-xiang |
| 2020,17(9):89-94 |
| Abstract(4315) View PDF(3499) |
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| Multi-axis Vibration Fatigue Life Prediction Based on Critical Plane |
| PEI Chen-hui, HE Huan, CHEN Guo-ping |
| 2020,17(9):95-99 |
| Abstract(4653) View PDF(3478) |
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| Acoustic Performance Test on Nacelle Inlet Composite Material Annular Acoustic Liner |
| GAO Xiang, XU Jian, XUE Dong-wen, YAN Qun, HUO Shi-yu |
| 2020,17(9):100-105 |
| Abstract(4609) View PDF(3640) |
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| Experiment on the Effect of Front-edge Jet on Cavity Noise Suppression |
| YAN Hao, HUANG Wen-chao, PAN Kai, LIU Xing-qiang |
| 2020,17(9):106-112 |
| Abstract(4671) View PDF(3486) |
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| Identification of Aircraft Skin Distributed Dynamic Load Based on Strain Modal Method |
| ZHANG Cong, FU Yi-zhan, LI Yuan-dong, LI Jia-xu |
| 2020,17(9):113-117 |
| Abstract(4801) View PDF(3498) |
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| Experimental Study on Equivalent Simplification of Buffeting Load Spectrum |
| SHI Yuan-hua, WANG Yong-jun |
| 2020,17(9):118-121 |
| Abstract(4406) View PDF(3550) |
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| Load Calculation of Drag Parachute for Fighter |
| CAI Zhi-jun, MIN Qiang, YU Ji-hong |
| 2020,17(9):122-128 |
| Abstract(4710) View PDF(3607) |
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| Ice Shedding Impact Analysis for Cabin Window of Civil Aircraft |
| LI Ting, LIANG Yuan, YANG Kai, FENG Si-dong |
| 2020,17(9):129-133 |
| Abstract(4272) View PDF(3517) |
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| Review and Prospect to the Development of Different Excitation Methods in Flutter Flight Test |
| JU Li-feng, KOU Bao-zhi |
| 2020,17(9):134-141 |
| Abstract(4664) View PDF(3522) |
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| Test Method of the Full State Examination of the Typical Hydraulic Pipeline of Aircraft |
| MIN Qiang, WANG Yong-yan, HUANG Hu, JIN Wei |
| 2020,17(9):142-148 |
| Abstract(4401) View PDF(3587) |
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| Simulation and Experimental Verification Composite Structure of Empennage Leading Edge against Bird Impact |
| KONG Ling-yong, LI Na, WU Zhi-bin |
| 2020,17(9):149-153 |
| Abstract(4445) View PDF(3449) |
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| Ditching Simulation and Model Test Technology of Large Transport Aircraft |
| LYU Jin-feng, LIANG Yuan, TAN Shen-gang |
| 2020,17(9):154-159 |
| Abstract(4609) View PDF(3482) |
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| Application of Flutter Flight Test Based on Time-frequency Analysis Method |
| WANG Shao-nan, LIU Li-kun |
| 2020,17(9):160-165 |
| Abstract(4202) View PDF(3503) |
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| Design and Implementation of Helicopter Flutter Flight Excitation System |
| LI Yu-li, KOU Bao-zhi, LIANG Hai-zhou |
| 2020,17(9):166-172 |
| Abstract(4774) View PDF(3537) |
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| Airworthiness Certification Technology on Civil Aircraft Fuel Tank Cover Withstanding the Engine Debris |
| #$TAB#$TABKONG Ling-yong, LU Jia-nan, WU Zhi-bin |
| 2020,17(9):173-179 |
| Abstract(4890) View PDF(3589) |
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| Experimenton Aircraft Panel under Simultaneous Action ofAcoustic Load and Hydrostatic Load |
| ZHANG Li, GUO Ding-wen, PAN Kai, LIU Zhi-hong |
| 2020,17(9):180-184 |
| Abstract(4569) View PDF(3459) |
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| Flight Test Investigation of Characteristics of Lateral Attenuation of Civil Aircraft Airworthiness Certification Noise |
| SONG Ya-hui, ZHANG Xiao-liang, ZHANG Yue-lin |
| 2020,17(9):185-193 |
| Abstract(4332) View PDF(3570) |
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| Appraisal Procedure for Mechanical Environment Adaptability DesignExternal Hanging System of Military Aircraft |
| LU Li-jin, SHEN Zu-hui |
| 2020,17(9):194-199 |
| Abstract(4454) View PDF(3566) |
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