Two-parameter model for delamination growth under mode i fatigue loading (Part A: Experimental study)

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
Research Group
Structural Integrity & Composites (Aerospace Engineering) (TU Delft)
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Published Date

2014

Language

English

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites