Root sizing criteria
In Flight Structural Loads. Sizing of Wing Box
Article REF: TRP4034 V1
Root sizing criteria
In Flight Structural Loads. Sizing of Wing Box

Author : Yves GOURINAT

Publication date: May 10, 2019 | Lire en français

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2. Root sizing criteria

2.1 Bottom panel

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2.1.1 Permissible stresses – Design principles

Remember that in a diaphragm, the flux (internal force per unit width) is also the product of the stress and the thickness (N YY = σ YY e skin , T YZ = τ YZ e spar ). Thus, the stresses...

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