Crashworthiness Optimization Design of Regional Airliner’s Fuselage Section Through Topometry Optimization
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
Funder
Key Research and Development Program of Shaanxi
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060049
Reference23 articles.
1. Crashworthiness Optimization of Aircraft Hybrid Energy Absorbers Enclosing Honeycomb and Foam Structures
2. Crushing analysis and multi-objective crashworthiness optimization of GFRP honeycomb-filled energy absorption devices
3. Research on Effects of Oblique Struts on Crashworthiness of Composite Fuselage Sections
4. The crashworthiness of civil aircraft using different quadrangular tubes as cabin-floor struts
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4. Crashworthiness optimization of thin-walled tube structures with tailor-welded blank using targeting force–displacement method;Structural and Multidisciplinary Optimization;2022-11-22
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