Reduced allowable strength of composite laminate for unknown distribution due to limited tests
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of Florida, USA
2. National Institute for Aviation Research, Wichita State University, USA
3. Materials Sciences Corporation, USA
Abstract
Funder
Defense Advanced Research Projects Agency
Publisher
SAGE Publications
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
http://journals.sagepub.com/doi/pdf/10.1177/0021998320903781
Reference32 articles.
1. Uncertainty modelling and code calibration for composite materials
2. Virtual calculation of the B-value allowables of notched composite laminates
3. Experimental evaluation and statistical characterization of the strength and strain energy density distribution of Kevlar KM2 yarns: exploring length-scale and weaving effects
4. Conservative Design Optimization of Laminated Composite Structures Using Genetic Algorithms and Multiple Failure Criteria
5. Application of bootstrap method in conservative estimation of reliability with limited samples
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1. Mechanical property distribution of composites considering cured ply thickness variability;Journal of Physics: Conference Series;2024-01-01
2. Design allowables of composite laminates: A review;Journal of Composite Materials;2022-08-04
3. Review of uncertainty quantification, associated parables, and Raphael Tuvia Haftka’s contributions;Structural and Multidisciplinary Optimization;2021-08-11
4. Reliability analysis using bootstrap information criterion for small sample size response functions;Structural and Multidisciplinary Optimization;2020-09-29
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