Hallo Engineers,(adsbygoogle = window.adsbygoogle || []).push({});

I am a little bit confused here and i need some guidance.

Can any of you educate me on how to calculate the Bending and Torsional stiffness of a Hat/Omega stringer attached on a plate to form a fuselage panel?..You can also recommend to me a book where it is clearly described so that i can get in-depth with the topic.

The material is Aluminium by the way.

Thank you guys in advance, i will really appreciate the help.

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# Aerospace Bending and Torsional stiffness of Hat/Omega stringer

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