Effect of stress ratio on delamination growth behavior in unidirectional carbon/epoxy undr mode I fatigue loading

Conference paper (2009)

Authors

R. Khan 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

2009

Language

Undefined/Unknown

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites