Impact test and numerical simulation of typical sub-cargo fuselage section of civil aircraft

Author:

Mou HaoleiORCID,Xie Jiang,Liu Yi,Cheng Kun,Feng Zhenyu

Funder

Aeronautical Science Foundation of China

Tianjin Municipal Education Commission Scientific Research Project

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference59 articles.

1. Research status and future development of crashworthiness of civil aircraft fuselage structures: an overview;Mou;Prog. Aerosp. Sci.,2020

2. Advances in crash dynamics for aircraft safety;Guida;Prog. Aerosp. Sci.,2018

3. Improvement of numerical methods for crash analysis in future composite aircraft design;Deletombe;Aerosp. Sci. Technol.,2000

4. Development of a finite element model for comparing metal and composite fuselage section drop testing;Gransden;Int. J. Crashworthiness,2017

5. An insight on the crashworthiness behavior of a full-scale composite fuselage section at different impact angles;Riccio;Aerospace,2019

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