Computational analysis demonstrates a weight-efficiency estimation algorithm for aircraft fuselage sections, highlighting structural gains from advanced composite lattice designs.
The results of forming a methodology and calculation algorithm to estimate the weight efficiency of fuselage sections with an advanced structure layout based on comparative analysis with alternative structure layouts are presented. Application of the developed methodology to estimate the weight efficiency of a lattice composite fuselage section of a passenger aircraft is shown.
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Dubovikov et al. (2019) studied this question.
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