Optimization of composite fuselage frame layup for energy absorption under crash loading

• Main Authors: Syed Mohamed Ali, Jaffar, M.J.A ., Muhammad Nazri
• Format: Article
• Language: English; English
• Published: Semarak Ilmu Publishing 2024
• Subjects: TA349 Mechanics of engineering. Applied mechanics; TL Motor vehicles. Aeronautics. Astronautics; TL500 Aeronautics
• Online Access: http://irep.iium.edu.my/113941/7/113941_Optimization%20of%20composite%20fuselage.pdf; http://irep.iium.edu.my/113941/13/113941_Optimization%20of%20composite%20fuselage_Scopus.pdf; http://irep.iium.edu.my/113941/; https://semarakilmu.com.my/journals/index.php/appl_mech/article/view/5090; https://doi.org/10.37934/aram.122.1.111129
• Institution: Universiti Islam Antarabangsa Malaysia

Considerable research has been carried out on aircraft fuselage design, with a particular focus on frames due to their role in energy absorption during crash impacts. While metallic alloys have traditionally been used for frame construction, the growing popularity of composites has led to a shift to...