Evaluation of BSAM (B-Spline Analysis Method) for Residual Strength and Life Prediction Using Three-Point Bend Doubler Under Quasi-Static and Cyclic Loading-Reference-Cited by-同舟云学术

Evaluation of BSAM (B-Spline Analysis Method) for Residual Strength and Life Prediction Using Three-Point Bend Doubler Under Quasi-Static and Cyclic Loading

Published:2020-01-05 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2020 Forum
language:
Short-container-title:

Author:

Selvarathinam Alex S.¹,Perera Shenal²,Smith Garrett²,Schaefer Joseph³,Johnston William⁴,Jackson Wade⁴,Rose Cheryl⁴,Obrien Thomas⁴

Affiliation:

1. Lockheed Martin Corporation

2. Wichita State University

3. The Boeing Company

4. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference15 articles.

1. Role of FEA, Closed-Form, and Empirical Models in Certifying Aircraft Composite Structures

2. Verification and Validation Process for Progressive Damage and Failure Analysis Methods in the NASA Advanced Composites Consortium

3. Assessment of Intralaminar Progressive Damage and Failure Analysis Methods Using an Efficient Evaluation Framework

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Fail-Safe Prediction for Bonded Composite Structures Using Discrete Damage Modeling;AIAA SCITECH 2023 Forum;2023-01-19

2. Progressive Damage Predictions of Composite Subelements Using Discrete Damage Modeling;AIAA SCITECH 2022 Forum;2022-01-03

3. Development of Analytical Capabilities for Through Thickness Composite Structure Design and Substantiation;AIAA SCITECH 2022 Forum;2022-01-03

4. Initiation and Propagation of Skin/Stiffener Separation in Postbuckled Structures Subjected to Cyclic Loads;AIAA Scitech 2021 Forum;2021-01-04

5. A Comparison of Discrete Damage Modeling Methods: The Effect of Stacking Sequence on Progressive Failure of the Skin Laminate in a Composite Pi-joint Subject to Pull-off Load;AIAA Scitech 2021 Forum;2021-01-04