Delamination in fiber metal laminates (GLARE) during fatigue crack growth under variable amplitude loading

Journal article (2011)

Authors

S.U. Khan Structural Integrity & Composites - Aerospace Engineering
René Alderliesten Structural Integrity & Composites - Aerospace Engineering
Rinze Benedictus Structural Integrity & Composites - Aerospace Engineering
Research Group
Structural Integrity & Composites (Aerospace Engineering) (TU Delft)
More Info
expand_more

Published Date

2011

Language

English

Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites