Creep under constant rivet pull through loading of a typical Glare skin-buttstrap connection. Test report

Report (2002)

Authors

V.P. Brügemann Structural Integrity & Composites - Aerospace Engineering
Research Group
Structural Integrity & Composites (Aerospace Engineering) (TU Delft)
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Published Date

2002

Language

Undefined/Unknown

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites