A Simple Test Method for Large Deformation Bending of Thin High Strain Composite Flexures
Author:
Affiliation:
1. NASA Langley Research Center
2. Opterus R&D, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0942
Reference24 articles.
1. Constrained buckling tests show increasing compressive strain to failure with increasing strain gradient
2. Compression Characterization of High-modulus Carbon Fibers
3. Folding of woven composite structures
4. Carbon Fibre Reinforced Plastic Tape Springs
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