Data Requirements for Progressive Damage Analysis of Double-Shear Bearing in Composites
Author:
Affiliation:
1. Lockheed Martin Corporation
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0736
Reference10 articles.
1. Engelstad SP, Stover RJ, Action JE, Air vehicle integration and technology research (AVIATR) Task Order 0037: Assessment, quantification, and benefits of applying damage tolerant design principles to advanced composite aircraft structure. AFRL Technical Report, Contract no. AFRL-RQ-WP-TR-2015-0068, February 2015.
2. Assessment of Composite Damage Growth Tools for Aircraft Structure - Part I
3. Assessment of Composite Damage Growth Tools for Aircraft Structure Part II
4. Data Requirements for Progressive Damage Analysis of Composite Structures
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