19th AIAA Applied Aerodynamics Conference 2001
DOI: 10.2514/6.2001-1193
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Curved flange effectivities for unsymmetric composites

Abstract: This paper presents closed form curved beam analysis, including unsymmetric and/or unbalanced composite material laminate effects, in beams with thin flanges. Flange effectivities and root transverse bending are presented in graphical form.

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