On the hysteretic response of mechanical strain induced by thermal stress in fastened metal-composite hybrid structures during a temperature cycle

Author:

Cong Zhiyuan,Yu Zhefeng,Jiang DongjieORCID

Funder

National Science Foundation of China

Publisher

Springer Science and Business Media LLC

Reference22 articles.

1. Goossens S, de Pauw B, Geernaert T et al (2019) Aerospace-grade surface mounted optical fibre strain sensor for structural health monitoring on composite structures evaluated against in-flight conditions. Smart Mater Struct 28(6):065008

2. Starikov R, Schn J (2001) Quasi-static behaviour of composite joints with protruding-head bolts. Compos Struct 51(4):411–425

3. McCarthy M (2003) BOJCAS: bolted joints in composite aircraft structures. Air Space Europe 3(3):139–142

4. Cai Q, Zhao Q (2021) Effects of temperature and clearance fit on the load distribution of composite-metal hybrid structures. Acta Mater Compos Sin 38(12):4228–4238

5. Fox DE, Swaim KW (1999) Static strength characteristics of mechanically fastened composite joints. NASA/TM-1999-209735

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