Knowledge based design method for fibre metal laminate fuselage panels
Conference Paper
(2005)
Author(s)
B Vermeulen (TU Delft - Structural Integrity & Composites)
Michel van Tooren (TU Delft - System Engineering & Aircraft Design)
L.J.B. Peeters (External organisation)
Research Group
Structural Integrity & Composites
To reference this document use:
https://resolver.tudelft.nl/uuid:d1fbd948-cd24-45a0-94bb-a4ec388bae02
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Publication Year
2005
Research Group
Structural Integrity & Composites
Pages (from-to)
1-10
ISBN (print)
0-7918-3766-1
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