Design of fibre metal laminate shear panels for ultra high capacity aircraft.

Journal article (2001)

Authors

TC Wittenberg Structural Integrity & Composites - Aerospace Engineering
TJ van Baten OLD Aerospace Structures
Research Group
Structural Integrity & Composites (Aerospace Engineering) (TU Delft)
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Published Date

2001

Language

Undefined/Unknown

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites