Continuous Tow Steering Around an Elliptical Cutout in a Composite Panel
Author:
Affiliation:
1. Airbus UK, Filton, Bristol, England BS34 7PA, United Kingdom
Funder
Science Foundation Ireland- Spatially and Temporally VARIable COMPosite Structure
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060668
Reference43 articles.
1. A general solution for stresses around holes in symmetric laminates under inplane loading
2. On the stress concentration around a hole in an infinite plate subject to a uniform load at infinity
3. Optimization in a Class of Hole Shapes in Plate Structures
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