Application of the strip-yield model from the NASGRO software to predict fatigue crack growth in aluminium alloys under constant and variable amplitude loading

Journal article (2007)

Authors

M. Skorupa External organisation
T. Machniewicz External organisation
J. Schijve Structural Integrity & Composites - Aerospace Engineering
A. Skorupa External organisation
Research Group
Structural Integrity & Composites (Aerospace Engineering) (TU Delft)
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Published Date

2007

Language

Undefined/Unknown

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites