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

A Vlot Structural Integrity & Composites - Aerospace Engineering
G. la Rocca Old - LR Ch. System Integration: Aircraft Design
Research Group
Structural Integrity & Composites (Aerospace Engineering) (TU Delft)
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Published Date

2001

Language

Undefined/Unknown

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites