Glare Technology Development 1997 - 2000

Journal article (2002)

Authors

J.W. Gunnink Structural Integrity & Composites - Aerospace Engineering
A Vlot Structural Integrity & Composites - Aerospace Engineering
T.J. de Vries Structural Integrity & Composites - Aerospace Engineering
W van der Hoeven External organisation
Research Group
Structural Integrity & Composites (Aerospace Engineering) (TU Delft)
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Published Date

2002

Language

Undefined/Unknown

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Faculty

Aerospace Engineering

Department

Aerospace Structures & Materials

Research Group

Structural Integrity & Composites

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.