56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015
DOI: 10.2514/6.2015-1879
|View full text |Cite
|
Sign up to set email alerts
|

Application of Reduced Order Multiscale Homogenization to ‘Assess and Quantify the Benefits of Applying Damage Tolerant Design Principles to Advanced Composite Aircraft Structures’

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2016
2016
2016
2016

Publication Types

Select...
1
1

Relationship

1
1

Authors

Journals

citations
Cited by 2 publications
(1 citation statement)
references
References 11 publications
0
1
0
Order By: Relevance
“…EHM can also account for progressive debonding between fiber and matrix at the scale of the microstructure, and is equipped with an adaptive model improvement capability to hierarchically increase model fidelity. 14 EHM has been successfully employed in the prediction of failure under static loading, 18,19 blast, 20 compression-after-impact, 21 and fatigue loading, 22 as well as failure in thin composite plates, 23,24 in the presence of environmental effects, 25 and in the presence of constituent material uncertainty. 26 In this manuscript, EHM is employed to predict the failure response of a suite of laminated, unidirectionally reinforced carbon fiber polymer (i.e., IM7/977-3) composite specimens subjected to static loading.…”
Section: Introductionmentioning
confidence: 99%
“…EHM can also account for progressive debonding between fiber and matrix at the scale of the microstructure, and is equipped with an adaptive model improvement capability to hierarchically increase model fidelity. 14 EHM has been successfully employed in the prediction of failure under static loading, 18,19 blast, 20 compression-after-impact, 21 and fatigue loading, 22 as well as failure in thin composite plates, 23,24 in the presence of environmental effects, 25 and in the presence of constituent material uncertainty. 26 In this manuscript, EHM is employed to predict the failure response of a suite of laminated, unidirectionally reinforced carbon fiber polymer (i.e., IM7/977-3) composite specimens subjected to static loading.…”
Section: Introductionmentioning
confidence: 99%