Knowledge based design method for fibre metal laminate fuselage panels

Conference paper (2005)

Authors

B Vermeulen Structural Integrity & Composites - Aerospace Engineering
M.J.L. van Tooren System Engineering & Aircraft Design
L.J.B. Peeters External organisation
Research Group
Structural Integrity & Composites (Aerospace Engineering) (TU Delft)
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Published Date

2005

Language

Undefined/Unknown

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites