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Buckling and Post-Buckling Analysis of a Composite Curved Structure

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Buckling and Post-Buckling Analysis of a Composite Curved Structure

 

In the nineties thin stiffened curved aerostructures were made in metal construction, by using thin plates with stiffeners profiles riveted. Other alternate solutions were discarded mainly due to manufacturing constraints. However, because the most critical failure mode of these structures was buckling, the optimisation addressed to an objective weight too high in comparison with other materials with higher Young’s modulus. The composite stiffened shape structures have come up once the main engineering problems (buckling, weight, ..) have been solved by the airframe world’s leader manufacturer as EADS CASA.

 

Authors: S. Ponce Borrero, F.J. Fernandez Sanchez, A. Gonzalez Diaz

Conference: SETEC 07 - Madrid, Spain - Sept. 6-7 / 2007

SKU/Code: SETEC 07 -05

Pages: 7

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