الرئيسية المصفحة

المصفحة

  • A Four-node Facet Shell Element for Laminated Shells Based on the Third Order Zigzag Theory

  • Design Allowable Considerations for use of Laminated Composites in Aircraft Structures

  • Effect of Boundary Conditions on Buckling Load for Laminated Composite Decks Plates

  • Review of Impact Damages Modelling in Laminated Composite Aircraft Structures

  • Effect of Aspect Ratio on Buckling Load for Laminated Composite Decks Plates