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15 June 2022, Volume 43 Issue 6

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15 June 2022, Volume 43 Issue 6

Reviews

Development status, challenges and trends of strength technology for hypersonic vehicles
Abstract( 4283 )

SUN Cong

doi: 10.7527/S1000-6893.2022.27590

2022, (6): 527590-527590.

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Development situation and future challenges of CAE software used in aeronautical structural analysis
Abstract( 1291 )

WANG Binwen, DUAN Shihui, NIE Xiaohua, GUO Yuchao

doi: 10.7527/S1000-6893.2022.27272

2022, (6): 527272-527272.

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Technological development in hypersonic nozzle design, manufacture and validation: A review
Abstract( 1165 )

LIN Peng, ZHUANG Fujian, QU Linfeng, XU Yangyang, SU Yadong

doi: 10.7527/S1000-6893.2022.26160

2022, (6): 526160-526160.

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Fundamental mechanical problems in high-performance aerospace composite structures: State-of-art review
Abstract( 2531 )

ZHAO Tian, LI Ying, ZHANG Chao, YAO Liaojun, HUANG Yixing, HUANG Zhixin, CHEN cheng, WANG Wandong, ZU Lei, ZHOU Huamin, QIU Jinhao, QIU Zhiping, FANG Daining

doi: 10.7527/S1000-6893.2022.26851

2022, (6): 526851-526851.

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Research progress on shimmy dynamics of aircraft landing gear systems
Abstract( 1288 )

LIU Xiaochuan, LIU Chongchong, MOU Rangke

doi: 10.7527/S1000-6893.2022.27063

2022, (6): 527063-527063.

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An overview of noise source control technology for helicopter main gearbox
Abstract( 653 )

ZHA Jianping, WANG Fengjiao, GUO Junxian, LI Mingqiang

doi: 10.7527/S1000-6893.2022.26123

2022, (6): 526123-526123.

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Research progress of collision safety characteristics of civil light and small UAVs
Abstract( 696 )

BAI Chunyu, GUO Yazhou, LIU Xiaochuan, WANG Yafeng, WANG Jizhen, QIN Qinghua

doi: 10.7527/S1000-6893.2022.26832

2022, (6): 526832-526832.

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Impact damage behavior of thin-ply composites: A review
Abstract( 1089 )

CAO Yong, ZHANG Chao

doi: 10.7527/S1000-6893.2021.25323

2022, (6): 525323-525323.

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Articles

Research and application of virtual test technology for static strength of full scale aircraft structure
Abstract( 786 )

WANG Binwen, NIE Xiaohua, WAN Chunhua, WU Cunli

doi: 10.7527/S1000-6893.2022.26273

2022, (6): 526273-526273.

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Damage recognition of composite structures based on domain adaptive model
Abstract( 705 )

WANG Yupeng, LYU Shuaishuai, YANG Yu, LI Jiaxin, WANG Yezi

doi: 10.7527/S1000-6893.2022.26752

2022, (6): 526752-526752.

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On the generalized survivability of aircraft and its evaluation method
Abstract( 586 )

HE Yuting

doi: 10.7527/S1000-6893.2022.26118

2022, (6): 526118-526118.

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Dynamic response of fuselage panel under explosive impact load
Abstract( 617 )

FENG Zhenyu, FU Boyu, XIE Jiang, DUAN Zhuxuan, PAN Hanyuan

doi: 10.7527/S1000-6893.2021.25513

2022, (6): 525513-525513.

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Dynamic response analysis of nose landing gear in aircraft new towing and taxiing mode
Abstract( 753 )

LI Yueming, LI Xiaoyun, CHAI Yijun, YANG Xiongwei

doi: 10.7527/S1000-6893.2022.26915

2022, (6): 526915-526915.

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Dynamic response analysis of nose landing gear in aircraft new towing and taxiing mode
Abstract( 104 )

LI Yueming, LI Xiaoyun, CHAI Yijun, YANG Xiongwei

doi: 10.7527/S1000-6893.2022.26915

2022, (6): 526915-526915.

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Acoustic performance experimental technology of aircraft nacelle acoustic liner
Abstract( 846 )

YAN Qun, XUE Dongwen, GAO Xiang, YANG Jiafeng, HUANG Wenchao

doi: 10.7527/S1000-6893.2022.26810

2022, (6): 526810-526810.

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Cracking behavior of thermal barrier coating after thermal shock based on perdynamic theory
Abstract( 733 )

MA Yu'e, YANG Meng, SUN Wenbo

doi: 10.7527/S1000-6893.2021.26587

2022, (6): 526587-526587.

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Acoustic emission monitoring technology for fatigue test of full-scale civil aircraft structure
Abstract( 722 )

YANG Yu, WANG Binwen, QI Xiaofeng

doi: 10.7527/S1000-6893.2022.27044

2022, (6): 527044-527044.

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Impact characteristics of typical sub-cargo structure of large aircraft: Tests and numerical simulation
Abstract( 602 )

XIE Jiang, MOU Haolei, FENG Zhenyu, CHENG Kun, LIU Yi, LIU Xiaochuan, BAI Chunyu, XI Xulong

doi: 10.7527/S1000-6893.2021.25890

2022, (6): 525890-525890.

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Effect of process-induced residual stress on strength of UAV composite wing
Abstract( 782 )

LIU Zhendong, ZHENG Xitao, FAN Wenjing, ZHANG Dongjian

doi: 10.7527/S1000-6893.2022.26117

2022, (6): 526117-526117.

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Evaluation of vibration caused discomfort in passenger aircraft cabin
Abstract( 923 )

LI Kaixiang, DAI Chenglin, ZHANG Fei, BAI Chunyu, MU Rangke

doi: 10.7527/S1000-6893.2022.25945

2022, (6): 525945-525945.

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Single-camera high-temperature three-dimensional digital image correlation method
Abstract( 604 )

YU Liping, PAN Bing

doi: 10.7527/S1000-6893.2022.27031

2022, (6): 527031-527031.

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Experiment on longitudinal dynamic impact characteristics of typical aircraft seat/occupant system
Abstract( 655 )

YANG Huan, LIU Xiaochuan, BAI Chunyu, ZHANG Yu, XI Xulong

doi: 10.7527/S1000-6893.2022.26238

2022, (6): 526238-526238.

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An equivalent strength model of corrugated panel and optimization design for morphing aircraft
Abstract( 576 )

WANG Chen, YANG Yang, SHEN Xing, XIA Yuying

doi: 10.7527/S1000-6893.2022.26146

2022, (6): 526146-526146.

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Flight test for gust alleviation on a high aspect ratio UAV platform
Abstract( 732 )

ZHOU Yitao, YANG Yang, WU Zhigang, YANG Chao

doi: 10.7527/S1000-6893.2022.26126

2022, (6): 526126-526126.

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Effect of preheating temperature on formation of surface cracks in thermal barrier coating system
Abstract( 586 )

LI Dingjun, YANG Liuyu, SUN Fan, JIANG Peng, CHEN Yiwen, WANG Tiejun

doi: 10.7527/S1000-6893.2021.26184

2022, (6): 526184-526184.

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A crack identification method of aircraft structure based on improved FaceNet
Abstract( 582 )

LYU Shuaishuai, YANG Yu, WANG Binwen, YIN Chenfei

doi: 10.7527/S1000-6893.2021.25463

2022, (6): 525463-525463.

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Analysis on CTOD corresponding parameters during fatigue crack growth
Abstract( 556 )

WANG Qiuyi, WU Yanzeng, BAO Rui

doi: 10.7527/S1000-6893.2022.26632

2022, (6): 526632-526632.

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Experimental study on crash characteristics of typical metal civil aircraft fuselage structure
Abstract( 588 )

ZHANG Xinyue, XI Xulong, LIU Xiaochuan, BAI Chunyu

doi: 10.7527/S1000-6893.2022.26234

2022, (6): 526234-526234.

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Braking vibration behavior of high strut landing gear of amphibious aircraft
Abstract( 519 )

DU Xiaoqiong, LI Bin, LUO Linyin

doi: 10.7527/S1000-6893.2022.26199

2022, (6): 526199-526199.

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Loading technology for main structure of large UAV durability test
Abstract( 492 )

CUI Ming, FENG Jianmin, MI Zheng, GUO Junhao

doi: 10.7527/S1000-6893.2022.25887

2022, (6): 525887-525887.

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Analysis method for damaged and fractured integral panel of large aircraft
Abstract( 515 )

ZHANG Zhinan, NING Yu, ZHUANG Zhuo, WANG Heng, QIN Jianbo, YAN Hong

doi: 10.7527/S1000-6893.2022.26134

2022, (6): 526134-526134.

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Static and fatigue test technology for full-scale composite fuselage barrels
Abstract( 546 )

GUO Qiong, LIU Wei, PEI Lianjie, GUO Junhao

doi: 10.7527/S1000-6893.2022.25816

2022, (6): 525816-525816.

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Hygrothermal vibration characteristics of repaired structures of laminates with penetrating damage
Abstract( 500 )

JIA Baohui, SHAN Jinyang, LU Xiang, WANG Du

doi: 10.7527/S1000-6893.2021.25518

2022, (6): 525518-525518.

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Design and validation of eccentric beam for variable camber trailing edge
Abstract( 614 )

ZHANG Sheng, YANG Yu, WANG Zhigang, SHI Xintong

doi: 10.7527/S1000-6893.2021.25892

2022, (6): 525892-525892.

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Probabilistic assessment on damage tolerance of composite helicopter horizontal tail structure
Abstract( 736 )

WAN Aoshuang

doi: 10.7527/S1000-6893.2021.25557

2022, (6): 525557-525557.

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Residual strength evaluation of curved hat-stiffened composite panels with discrete-source damage
Abstract( 487 )

WANG Houbing, WANG Xiahan, LIN Guowei, LI Xinxiang, YANG Shengchun

doi: 10.7527/S1000-6893.2022.25899

2022, (6): 525899-525899.

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Response characteristics of sandwich structure with S-shaped CFRP folded core under low velocity impact
Abstract( 553 )

DENG Yunfei, ZHOU Nan, TIAN Rui, WEI Gang

doi: 10.7527/S1000-6893.2021.25446

2022, (6): 525446-525446.

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Test technology for complex stress field of large scale fuselage panel
Abstract( 470 )

LI Chong, CHAI Yanan, WANG Binwen, CHEN Xiangming, YU Zhenbo, ZHOU Hong

doi: 10.7527/S1000-6893.2022.26409

2022, (6): 526409-526409.

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Crashworthiness design of bio-inspired ring arrays for impact protection
Abstract( 403 )

XING Yun, ZHANG Qiao, YANG Xianfeng, LIU Hua, YANG Jialing

doi: 10.7527/S1000-6893.2021.26194

2022, (6): 526194-526194.

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Follow-up loading technology for lift structure with spatial complex movement
Abstract( 492 )

ZHANG Tuo, SONG Pengfei, YIN Wei, DU Xing, REN Peng

doi: 10.7527/S1000-6893.2022.26044

2022, (6): 526044-526044.

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Acoustic design and experimental verification of full-scale nacelle exhaust duct liner
Abstract( 616 )

HUO Shiyu, YANG Jiafeng, DENG Yunhua, YAN Qun

doi: 10.7527/S1000-6893.2022.26736

2022, (6): 526736-526736.

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Effect of yarn size on tensile properties of 3D woven composites
Abstract( 852 )

LIU Zengfei, LIU Kai, ZHANG Binbin, LI Xuefeng, GE Jingran, HUANG Jian, LI Chao, SUN Xinyang, SUN Yu, LIANG Jun

doi: 10.7527/S1000-6893.2021.25453

2022, (6): 525453-525453.

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Total visits: 6658907 Today visits: 1341