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
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
Englisch
Buckling of composite panels: A criterion for optimum stiffener design
Online Contents | 2012
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