Design Tailoring for Pressure Pillowing Using Tow-Placed Steered Fibers
Author:
Affiliation:
1. Delft University of Technology, 2629 HS Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.32676
Reference16 articles.
1. Compression Buckling Response of Tailored Rectangular Composite Plates
2. Shear buckling response of tailored composite plates
3. Composite laminates with spatially varying fiber orientations - 'Variable stiffness panel concept'
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