基于ANSYS的复合材料层合板单钉连接件参数化结构仿真

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2006, Vol. 27 ›› Issue (6): 1088-1091.

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Parameterized Simulation for Composite Laminates with Single Mechanically Fastened Joint Based on ANSYS

ZHANG Shuang¹, WANG Dong¹, LI Zheng-neng¹, KOU Chang-he¹, ZHANG Yi-ning²

1. Aircraft Design and Research Institute, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;2. Shenyang Aircraft Design and Research Institute, Shenyang 110035, China

Received:2005-05-26 Revised:2005-11-30 Online:2006-12-25 Published:2006-12-25

Abstract

Abstract: A parameterized simulation program is developed to predict the response of composite laminates with single bolt structure. The three-dimensional non-linear progressive damage model is developed on the platform of ANSYS using APDL. Parameterized modeling and progressive damage simulation could be achieved in this analysis. The analysis takes into account the contact at bolt-hole interface. The effects of stacking sequences and geometrical parameters on the bearing strength are determined experimentally. For all the analyses performed, the damage progression of single bolted joint is predicted.

Key words: structure simulation, composite laminates, mechanically joints, progressive damage, contact model

CLC Number:

V229+.7

ZHANG Shuang;WANG Dong;LI Zheng-neng;KOU Chang-he;ZHANG Yi-ning. Parameterized Simulation for Composite Laminates with Single Mechanically Fastened Joint Based on ANSYS[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(6): 1088-1091.

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Parameterized Simulation for Composite Laminates with Single Mechanically Fastened Joint Based on ANSYS

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