2021
DOI: 10.2514/1.j060049
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Crashworthiness Optimization Design of Regional Airliner’s Fuselage Section Through Topometry Optimization

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Cited by 6 publications
(2 citation statements)
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“…The desired FD response is achieved; several crashworthiness indicators are improved simultaneously such as peak force, mean force, specific energy absorption, and crash load efficiency. Nowadays, the TFD method is applied to crashworthiness optimization design of automobile front structures [30] and regional airliner's fuselage section [31] successfully. Although the idea of optimizing the thicknesses of each (shell) finite element of the structure gets good optimization results, this idea led to poor manufacturability of the designed structure.…”
Section: Introductionmentioning
confidence: 99%
“…The desired FD response is achieved; several crashworthiness indicators are improved simultaneously such as peak force, mean force, specific energy absorption, and crash load efficiency. Nowadays, the TFD method is applied to crashworthiness optimization design of automobile front structures [30] and regional airliner's fuselage section [31] successfully. Although the idea of optimizing the thicknesses of each (shell) finite element of the structure gets good optimization results, this idea led to poor manufacturability of the designed structure.…”
Section: Introductionmentioning
confidence: 99%
“…This method is employed in a variety of sheet metal constructions to improve the mechanical properties. [30][31][32][33] In the authors' previous study, [34] free-size optimization-based graded lattice generation (FOGLG) is applied successfully for the first time to surface-based DG lattice structure. The performance of the proposed method is compared with HMTO in terms of modal response to demonstrate its effectiveness.…”
mentioning
confidence: 99%