Application of a modified Wheeler model to predict fatigue crack growth in fibre metal laminates under variable amplitude loading

Journal article (2010)

Authors

S.U. Khan Structural Integrity & Composites - Aerospace Engineering
R.C. Alderliesten Structural Integrity & Composites - Aerospace Engineering
C.D. Rans 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

2010

Language

English

Reuse Rights

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites