摘要 |
Disclosed is a fuselage 2 of a fibre-reinforced composite material for an aircraft with a skin 4 and with a multiplicity of circumferential stiffeners 12 and only a small number of longitudinal stiffeners 10, wherein the skin 4 has a multiplicity of local reinforcements 14; also disclosed is a skin field 6 for purposes of forming such a fuselage.
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