Design of fibre metal laminate shear panels for ultra high capacity aircraft.
Journal Article
(2001)
Author(s)
TC Wittenberg (TU Delft - Structural Integrity & Composites)
TJ van Baten (TU Delft - OLD Aerospace Structures)
Research Group
Structural Integrity & Composites
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https://resolver.tudelft.nl/uuid:e0f5c124-81ef-4d30-a396-c74c5babc035
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Publication Year
2001
Research Group
Structural Integrity & Composites
Issue number
2-3
Volume number
2001
Pages (from-to)
99-113
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