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Structural Limits

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timmayb67

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Hello Everyone,
I'm putting back together a one of one biplane and was wondering what actually determines the ultimate strength of a wing design besides the spar size.
Also, is there a strength advantage to the Pitts/Skybolt single attach point for the upper wing to the fuselage vs. A double mount like a Miniplane/Acrosport/Starduster style?
 

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