Glare Technology Development 1997 - 2000

Journal Article (2002)
Author(s)

J.W. Gunnink (TU Delft - Structural Integrity & Composites)

A Vlot (TU Delft - Structural Integrity & Composites)

TJ de Vries (TU Delft - Structural Integrity & Composites)

W van der Hoeven (External organisation)

Research Group
Structural Integrity & Composites
More Info
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Publication Year
2002
Research Group
Structural Integrity & Composites
Volume number
9
Pages (from-to)
201-219

Abstract

Fibre Metal Laminates (e.g. Glare) are composed of a bonded structure of metalic layers and fibre reinforced adhesive layers and were developed by laboratory testing and design during the last fifteen years. The Glare Technology Development (GTO) has been aiming at final technology readiness for application in aircraft design, production and service. The current paper gives an overview of the work that was done in this large project.

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