@inproceedings{1e4050a2ac1a48508b415d610f36aff4,
title = "Impact resistance research of composite laminate structure",
abstract = "The composite material has been widely used in aircraft structures. But this kind of material has some shortage such as poor impact resistance, low residual compressive strength, which have a negative influence on the performance of aircraft structures. In this paper, simulations of low-velocity impact and compression process of composite laminates with AL ply and different core material has been done. The simulation results show that softer core materials and AL ply with certain thickness can improve the residual compressive strength.",
keywords = "Fiber-metal laminate, Low velocity impact, Residual compressive strength, Sandwich composite laminate",
author = "Li, \{Hong Peng\} and Li Shu and Huang, \{Fang Lue\}",
year = "2013",
doi = "10.4028/www.scientific.net/AMR.712-715.1045",
language = "英语",
isbn = "9783037857243",
series = "Advanced Materials Research",
pages = "1045--1049",
booktitle = "Advances in Manufacturing Science and Engineering",
note = "4th International Conference on Manufacturing Science and Engineering, ICMSE 2013 ; Conference date: 30-03-2013 Through 31-03-2013",
}