For this study, structural and manufacturing schemes for low-curvature pressurized\nfuselage panels were proposed, making it possible to provide high weight efficiency for the airframes\nof prospective civil blended wing-body (BWB) aircraft. The manufacturing scheme for low-curvature\npanels helped to achieve high strength characteristics of the composite details as well as decreased\nthe labor input necessary for manufacturing and assembling. The beneficial features of the proposed\nstructure are that the panels have a low weight, incur low manufacturing costs, and satisfy the\ndemands of repairability.
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