Geometric design and mechanical properties of cylindrical foldcore sandwich structures by Zhou, X, Zang, S, Wang, H, You, Z

“…The design protocol together with the virtual test results can serve as a useful tool for researchers to design cylindrical foldcore sandwich structures for many potential applications including but not limited to aircraft fuselage, submarine shell and other pressurized cylinders. …”

Eco-efficient lightweight carbon-fiber reinforced polymer for environmentally greener commercial aviation industry by Khalil, Y

“…This research aims to perform comparative impact assessment for production of conventional aluminum alloy (AlMg3) used in aircraft fuselage and lighter weight carbon-fiber reinforced polymer (CFRP). …”

The evolution of electrochemical, microstructural, and mechanical properties of aluminium alloy 2024-T4 (D16AT) during fatigue cycling by Salimon, SR, Salimon, A, Korsunsky, A

“…Coupons of fuselage skin made from the aluminium alloy D16AT (the Russian equivalent of 2024-Ò4) were obtained from several Russian TU-154 passenger aircraft after different numbers of flight cycles and different lengths of operation. …”

FIB-SEM investigation of laser-induced periodic surface structures and conical surface microstructures on D16T (AA2024-T4) alloy by Salimon, I, Mailis, S, Salimon, A, Korsunsky, A

“…The use of aluminum alloy AA2024-T4 (Russian designation D16T) in applications requiring a high strength-to-weight ratio and fatigue resistance such as aircraft fuselage often demands the control and modification of surface properties. …”

The evolution of electrochemical, microstructural, and mechanical properties of aluminium alloy 2024-T4 (D16AT) during fatigue cycling by Salimon, S, Salimon, A, Korsunsky, A

“…Coupons of fuselage skin made from the aluminium alloy D16AT (the Russian equivalent of 2024-Ò4) were obtained from several Russian TU-154 passenger aircraft after different numbers of flight cycles and different lengths of operation. …”