Loads applied to the wing
In Flight Structural Loads. Sizing of Wing Box
Article REF: TRP4034 V1
Loads applied to the wing
In Flight Structural Loads. Sizing of Wing Box

Author : Yves GOURINAT

Publication date: May 10, 2019 | Lire en français

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1. Loads applied to the wing

1.1 External loads

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1.1.1 Structural box

The wing of a subsonic transport aircraft has a number of movable surfaces at the leading edge (deployable slats) and trailing edge (flaps and ailerons). The fixed, central structural portion forms the primary wing box (figure 1 ).

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