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Design and build of panels with large cut-outs under tension and shear

Description: This project was part of the new concepts development program in Fokker Aerostructures. The design of the rectangular panels in KM Perspektiva II was improved, three panels were built with Automated fibre placement using prepreg thermoset materials and will be tested in the Aerospace Structures and Materials Laboratory of Delft University of Technology.

Read the full documentation and case study:icon Design of Non-Conventional Laminates 

 

funded by: Fokker Aerostructures
manufacturing subcontract with: NLR
testing with: Delft University of Technology

 

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