Maximum buckling load design and post-buckling compressive failure of curved grid sub-stiffened composite panels
Author:
Funder
National Engineering School of Tunis
Publisher
Elsevier BV
Reference65 articles.
1. Design of variable stiffness composite panels for maximum fundamental frequency using lamination parameters;Abdalla;Compos. Struct.,2007
2. Optimal design of tow-placed fuselage panels for maximum strength with buckling considerations;Alhajahmad;J. Aircraft,2010
3. Minimum weight design of curvilinearly grid-stiffened variable-stiffness composite fuselage panels considering buckling and manufacturing constraints;Alhajahmad;Thin-Walled Struct.,2021
4. Design tailoring of curvilinearly grid-stiffened variable-stiffness composite cylindrically curved panels for maximum buckling capacity;Alhajahmad;Thin-Walled Struct.,2020
5. Buckling performance of curvilinearly grid-stiffened tow-placed composite panels considering manufacturing constraints;Alhajahmad;Compos. Struct.,2020
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