复合材料和结构机械连接件破坏历程的数值模拟与试验验证

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1995, Vol. 16 ›› Issue (2): 16-20.

• 论文 • Previous Articles Next Articles

NUMERICAL SIMULATION AND EXPERIMENTAL VERIFICATION OF FAILURE PROCESS AND LOAD-CARRYING CAPACITY FOR MECHANICALLY FASTENED JOINTS IN COMPOSITE MATERIALS AND STRUCTURES

Guan Changwen¹, Chen Haoran¹, Zheng Changlian¹

1. Dlian University of Technology, Dalian,116023; 2. Shenyang Aircraft Manufacture Company,Shenyang,11075

Received:1994-04-14 Revised:1994-07-20 Online:1995-04-25 Published:1995-04-25

Abstract

Abstract: The bolt load distribution,progressive failure models and corresponding load-carrying capacity for mechanically fastened joints in composite materials and structures are investigated by means of numerical simulation combined with experimental verification.The theoretical and experimental results for typical joints as examples are in good agreement,illustrating the effectiveness of the numerical simulation provided in the paper.

Key words: digital simulat ion, loadcarrying capacity, experimental verificat ion

CLC Number:

Guan Changwen;Chen Haoran;Zheng Changlian. NUMERICAL SIMULATION AND EXPERIMENTAL VERIFICATION OF FAILURE PROCESS AND LOAD-CARRYING CAPACITY FOR MECHANICALLY FASTENED JOINTS IN COMPOSITE MATERIALS AND STRUCTURES[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1995, 16(2): 16-20.

[1]	. Dynamics modeling and validation of L-shaped pipeline in aero-engine subjected to base random vibration excitation and fluid pressure pulsation excitation loads [J]. Acta Aeronautica et Astronautica Sinica, 0, (): 0-0.
[2]	. Modeling research of dielectric properties of graphene-doped polymer composites [J]. Acta Aeronautica et Astronautica Sinica, 0, (): 0-0.
[3]	Yankuan LIU, Hang YUAN, Dinghe LI, Yujie FEI. Effect of thermal aging on mechanical properties of thermal barrier coatings interface and numerical calculation [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(20): 428507-428507.
[4]	Tianchun ZOU, Yuezhang JU, Yuxi GUAN, Zegang LI, Hongcheng CHEN. Effect of stacking sequence on fatigue behavior of CFRP⁃Al joint [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(18): 428264-428264.
[5]	Yongsheng YE, Di DING, Haihua WU, Enyi HE, Shihao YIN, Zhenglang HU, Chao YANG. Graphene-enhanced Fe₃O₄/ethylcellulose composite microspheres with wave absorption properties [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(11): 427549-427549.
[6]	Yu WANG, Hongda XU, Hao LI, Chang LI. Vibration analysis of rotating dual⁃functional gradient composite cylindrical shell reinforced with carbon nanotubes [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(13): 227827-227827.
[7]	LI Hui, LYU Haiyu, ZOU Zeyu, LUO Zhong, MA Hui, HAN Qingkai. Analysis and verification of nonlinear vibrations of fiber-reinforced composite cylindrical shells in thermal environment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 425642-425642.
[8]	ZOU Tianchun, LI Longhui, LIU Zhihao, FU Ji, JU Yuezhang. Effect of overlap length on strain distribution and failure law of CFRP-Al double lap joint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 224921-224921.
[9]	TONG Anshi, XIE Liyang, BAI Enjun, BAI Xin, ZHANG Shijian, WANG Bowen. Test and prediction model of statics property of fiber metal laminates [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(11): 221193-221193.
[10]	XU Qi, WU Zhen. A Reddy-type theory of functionally graded beam considering transverse normal thermal strain [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(8): 220918-220918.
[11]	WANG Yan, LI Shu, XU Qiuyi, MA Jun. Optimization design and analysis of stiffened composite panels in post-buckling under shear [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(5): 1512-1525.
[12]	MENG Weiying, XIE Liyang, LIU Jianzhong, BAI Xin, TONG Anshi. Contrast study on fatigue life performance of glass fiber reinforced Al-Li alloy laminates under unimodal overload [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(5): 1536-1543.
[13]	SHI Youan, HE Lixin, QIU Bo, ZENG Lei, GENG Xiangren, WEI Dong. Multiscale heat transfer analysis of Z-directional carbon fiber reinforced braided composites [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(4): 1207-1217.
[14]	DAI Jixiang, SHA Jianjun, WANG Shouhao, WANG Yongchang. Influence of fiber surface state on microstructure and phase composition of C/C-SiC composites [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(5): 1704-1712.
[15]	LI Biao, LI Yazhi, Yang Fan. Theoretical Methodology for Laminated Composite Strength Including In-situ Effect [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(11): 3025-3036.

NUMERICAL SIMULATION AND EXPERIMENTAL VERIFICATION OF FAILURE PROCESS AND LOAD-CARRYING CAPACITY FOR MECHANICALLY FASTENED JOINTS IN COMPOSITE MATERIALS AND STRUCTURES

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments