Buckling-optimized variable stiffness laminates for a composite fuselage window section

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TP-2012-313.pdf (4.16 MB)
Date
2012
Authors
Brink, W.M. van den
Vankan, W.J.
Maas, R.
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National Aerospace Laboratory NLR
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http://hdl.handle.net/10921/932
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