Validation of Floating Node Method Using Three-Point Bend Doubler Under Quasi-Static Loading
Author:
Affiliation:
1. Lockheed Martin Corporation
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1549
Reference16 articles.
1. Role of FEA, Closed-Form, and Empirical Models in Certifying Aircraft Composite Structures
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