Multi-Scale Nonlinear Progressive Damage and Failure Analysis for Open-Hole Composite Laminates
In order to study the nonlinear behaviors and interactions among the constituents for the composite material structure under the tensile load, multiscale damage model using generalized method of cells (GMC) and a lamina-level progressive damage model were established, respectively, for fiber reinfor...
Main Authors: | Jian Shi, Mingbo Tong |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2022-01-01
|
Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/9/2/59 |
Similar Items
-
Progressive Damage Based Failure Analysis of Open-hole Composite Laminates under Tension
by: LI Rupeng, et al.
Published: (2018-10-01) -
Progressive Failure Analysis in Open-Hole Tensile Composite Laminates of Airplane Stringers Based on Tests and Simulations
by: Jian Shi, et al.
Published: (2020-12-01) -
Progressive Failure Analysis of Laminates with Embedded Wrinkle Defects Based on an Elastoplastic Damage Model
by: Zhi Hua Ning, et al.
Published: (2020-05-01) -
Mori–Tanaka Formalism-Based Method Used to Estimate the Viscoelastic Parameters of Laminated Composites
by: Mostafa Katouzian, et al.
Published: (2020-10-01) -
Progressive failure analysis for impact damage and compressive strength of composite laminates
by: Yukihiro SATO, et al.
Published: (2017-07-01)