Shear buckling of aerospace panels made by induction welded thermoplastic matrix composite elements
Author:
Affiliation:
1. Department of Engineering for Innovation University of Salento Lecce Italy
2. Advanced Materials and Processes Consulting CETMA‐Technologies Design and Materials European Research Centre Brindisi Italy
Publisher
Wiley
Subject
Materials Chemistry,Polymers and Plastics,General Chemistry,Ceramics and Composites
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/pc.26711
Reference32 articles.
1. Megson T.H.G.:Aircraft structures for engineering students: Sixth edition. Elsevier Inc. (2016). ISBN 9780081009147; 253–324.
2. Buckling, postbuckling, and failure of stiffened panels under shear and compression
3. Effect of in-plane fiber waviness defects on the compressive properties of quasi-isotropic thermoplastic composites
4. Design of fiber metal laminate shear panels for ultra-high capacity aircraft
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