Buckling and postbuckling performance of composite fuselage panels with cutouts using continuous streamline fibres

Author:

Alhajahmad Ahmad,Mittelstedt Christian

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Civil and Structural Engineering

Reference41 articles.

1. Tow-Placement Technology and Fabrication Issues for Laminated Composite Structures;Gürdal,2005

2. Curvilinear variable stiffness 3D printing technology for improved open-hole tensile strength;Khan;Addit. Manuf.,2018

3. In-plane response of laminates with spatially varying fiber orientations: Variable stiffness concept;Gürdal;AIAA Journal,1993

4. Design tailoring for pressure pillowing using tow-placed steered fibers;Alhajahmad;AIAA Journal of Aircraft,2008

5. Framework for the buckling optimization of variable-angle tow composite plates;Wu;AIAA J,2015

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