Energy-Release Rate and Mode Mixity of Face/Core Debonds in Sandwich Beams-Reference-Cited by-同舟云学术

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Energy-Release Rate and Mode Mixity of Face/Core Debonds in Sandwich Beams

Published:2013-04 Issue:4 Volume:51 Page:885-892
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Kardomateas George A.¹,Berggreen Christian²,Carlsson Leif A.³

Affiliation:

1. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332-0150

2. Department of Mechanical Engineering, Technical University of Denmark, 2800 Lyngby, Denmark

3. Department of Mechanical Engineering, Florida Atlantic University, Boca Raton, Florida 33431

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J051765

Reference15 articles.

1. The Initial Post-buckling Behavior of Face-Sheet Delaminations in Sandwich Composites

2. Buckling and postbuckling of delaminated composites under compressive loads including transverse shear effects

3. Large deformation effects in the postbuckling behavior of compositeswith thin delaminations

4. The Energy-Release Rate in the Growth of a One-Dimensional Delamination

5. Interface crack between two elastic layers

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2. A combined interface phase field (CIPF) model for interfacial crack propagation;Engineering Fracture Mechanics;2024-01

3. Mixed Mode Fracture Mechanics Characterization of DCB-UBM Sandwich Specimen Under Dynamic Loading;Procedia Structural Integrity;2024

4. Timoshenko Theory Solution for the Debond Characteristics of Sandwich Single-Cantilever-Beam Specimens;AIAA Journal;2023-09-04

5. Large Deflection Effects on the Energy Release Rate and Mode Partitioning of the Single Cantilever Beam Sandwich Debond Configuration;Journal of Applied Mechanics;2023-08-25

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