Size and shape optimization of aluminum tubes with GFRP honeycomb reinforcements for crashworthy aircraft structures. (1st December 2015)

• Record Type: Journal Article
• Authors: Paz, J.; Díaz, J.; Romera, L.; Costas, M.
• Is Part Of: Composite structures. Volume 133(2016)
• Page Start: 499
• Page End: 507
• Publication Date: 2015-12-01
• Subjects: Crashworthiness -- Multi-objective optimization -- Surrogate methods -- Honeycomb structure -- GFRP; Composite construction -- Periodicals; Composites -- Périodiques; 624.18
• DOI: 10.1016/j.compstruct.2015.07.077
• Languages: English
• ISSNs: 0263-8223

Abstract

Abstract: Crashworthiness optimization of aircraft and automotive structures has become one the main research targets for their respective leading industries. The following research proposes a new design of an aircraft's vertical strut. The design consists of a hollow aluminum square tube with a glass-fiber reinforced polymer honeycomb-shaped inner structure. Size and shape surrogate-based optimization techniques are used, with the thicknesses of both materials, cell size and cell shape as design variables. The objective function chosen for the single-objective optimization is the specific energy absorption, while the metrics for the multi-objective optimization are the peak force, mass, absorbed energy and the specific energy absorption. An improvement of 22% of the specific energy absorption with low peak force values is obtained from the single-objective optimization by significantly changing all design variables. Two Pareto fronts have been obtained from the multi-objective optimization confronting, the specific energy absorption against the peak force and the mass against the energy absorbed. When compared to the baseline model, the optimized models show substantial improvement, increasing the specific energy absorption by 65% or reducing the peak force by over 55%. It has been observed an important effect of the cell shape on the model's performance.