Development of a hybrid material for aerospace application, made of C/E sandwich panels with Glare protection. An experimental evaluation of the impact behaviour.

Journal article (2001)

Authors

G. la Rocca Old - LR Ch. System Integration: Aircraft Design
A Vlot Structural Integrity & Composites - Aerospace Engineering
A Frediani External organisation
Research Group
Old - LR Ch. System Integration: Aircraft Design
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Published Date

2001

Language

Undefined/Unknown

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Research Group

Old - LR Ch. System Integration: Aircraft Design