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

Khan, S.U.; Alderliesten, R.C.; Rans, C.D.; Benedictus, R.

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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http://resolver.tudelft.nl/uuid:0eabe547-b89a-4bfd-9c61-73bb13da4876

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Published Date

2010

Language

English

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites