A

A Vlot

50 records found

Authored

From Laboratory Material Development to Industrial application for Fibre Metal Laminates.

Fibre Metal Laminates as a damage tolerant material for aircraft structures.
Conference paper (2001) - A Vlot

The behaviour of Glare material after severe impact in a row of holes or rivet row containing flaws and fatigue damage.
Conference paper (2001) - T.J. de Vries, PA Hooijmeijer, A Vlot

Influence of surface pretreatment when determining the shear stress-strain relationships of structural adhesives.
Conference paper (2001) - H Botter, A van den Berg, F Soetens, IJJ van Straalen, A Vlot

Historical Overview
Conference paper (2001) - A Vlot

We are people of the way.
Journal article (2001) - A Vlot, B Goudzwaard

Feasibility study for Glare as pressure bulkhead material.
Report (2001) - A Vlot

Het luchtschip als freighter: verkenningen naar milieubelasting en duurzaamheid en markttoepassingen bij KLM Cargo.
Report (2001) - A Vlot

Repair of fibre metal laminates.
Conference paper (2001) - PA Hooijmeijer, A Vlot

Adhesive bonded nodes in automotive spaceframes.
Report (2001) - A Vlot

Het koud oprekken van gaten in Glare.
Report (2001) - A Vlot

Cultural diversity and technological development.
Journal article (2001) - A Vlot

Environmental influence on GLARE riveted joints.
Conference paper (2001) - T Beumler, A Vlot, O Kieboom, B Borgonje

Durability of bonded fibre metal laminate repair patches.
Conference paper (2001) - HJM Woerden, A Vlot, R Brenninkmeijer

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) - G. la Rocca, A Vlot, A Frediani

Feasibility study for life enhancement of military aircraft through re squeezing joints with geriatric aircraft.
Report (2001) - RPG Mueller, A Vlot, JJ Homan

Verification of a design method for stiffened panels loaded in shear.
Report (2001) - A Vlot

Development of a fatigue crack growth model for surface cracks in Glare.
Report (2001) - KAM Gonesh, A Vlot

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) - A Vlot, G. la Rocca

Development of a hybrid material for aerospace application made of C/E sandwich panels with GLARE Protection and experimental evaluation of impact behaviour.
Conference paper (2001) - G. la Rocca, A Vlot