Postbuckled behavior of composite isogrid stiffened shell structure
Author:
Publisher
Informa UK Limited
Subject
Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
http://www.tandfonline.com/doi/pdf/10.1163/15685510051033467
Reference7 articles.
1. Continuous filament wound composite concepts for aircraft fuselage structures
2. Kim, T. and Rotz, C. Warping of flat composite isogrid panels. 1997 IEEE Aerospace Conference. pp.271–277. Aspen
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