Design optimisation procedure for fibre metal laminates based on fatigue crack initiation

Journal article (2015)

Authors

I. Şen 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

2015

Language

English

Reuse Rights

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites