Crashworthiness analysis of an aircraft fuselage section with an auxiliary fuel tank using a hybrid multibody/plastic hinge approach
Author:
Affiliation:
1. Department of Mechanical Engineering, Wichita State University, Wichita, KS, USA;
2. Department of Mechanical Engineering, University of Minho, Guimarães, Portugal
Publisher
Informa UK Limited
Subject
Industrial and Manufacturing Engineering,Mechanical Engineering,Transportation
Link
https://www.tandfonline.com/doi/pdf/10.1080/13588265.2018.1524547
Reference10 articles.
1. A modern aerospace modeling approach for evaluation of aircraft fuselage crashworthiness
2. Scale modelling of aircraft fuselage: an innovative approach to evaluate and improve crashworthiness
3. Improvement of crashworthiness behaviour for simplified structural models of aircraft fuselage
4. Integration of a Composite Crash Absorber in Aircraft Fuselage Vertical Struts
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