Failure criterion for the skin-stiffener interface in composite aircraft panels
1998
33 S
Ill., graph. Darst
This report is based on an article to be published in the proceedings of the Thirteenth Technical Conference of the American Society for Composites
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Buckling of composite panels: A criterion for optimum stiffener design
Online Contents | 2012
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