Crack closure and fibre bridging during delamination growth in carbon fibre/epoxy laminates under mode I fatigue loading

Journal article (2014)

Authors

R. Khan Structural Integrity & Composites - Aerospace Engineering

R.C. Alderliesten Structural Integrity & Composites - Aerospace Engineering

R. Benedictus Structural Integrity & Composites - Aerospace Engineering

L. Yao Structural Integrity & Composites - Aerospace Engineering

Research Group

Structural Integrity & Composites (Aerospace Engineering) (TU Delft)

More Info

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http://resolver.tudelft.nl/uuid:f1b66942-b8fd-4bf1-bc43-5ccf773e4df2

Published Date

2014

Language

English

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites