Results 101 to 110 of about 13,057 (258)

Predicting fatigue crack initiation in fibre metal laminates based on metal fatigue test data [PDF]

, 2015
Alderliesten, RC, Sen, I, Spronk, Siebe
core   +1 more source

Application of fiber bridging models to fatigue crack growth in unidirectional titanium matrix composites [PDF]

Several fiber bridging models were reviewed and applied to study the matrix fatigue crack growth behavior in center notched (0)(sub 8) SCS-6/Ti-15-3 and (0)(sub 4) SCS-6/Ti-6Al-4V laminates.
Bakuckas, J. G., Jr., Johnson, W. S.
core   +1 more source

A study of repeated impact loading on a symmetrical carbon fibre laminate [PDF]

, 2007
The behaviour of a symmetric laminate under repeated low energy hits of a 12.1mm hemispheric impactor was evaluated. The laminate was able to endure 20 collisions with the striker before perforation. The rate of damage progression was characterised by an
Banks, W.M., David-West, O.S., Nash, D.H.   +2 more
core  

Experimental Analysis of Fibre Metal Laminates

IOP Conference Series: Materials Science and Engineering, 2018
D Giridharan, Bhupal Rakham
openaire   +1 more source

The Effect of Self-Healing Microcapsules in Corrosion Testing on Magnesium AZ31 Alloy and Fibre Metal Laminates [PDF]

Monika Ostapiuk, J. Bieniaś, Mónica V. Loureiro, Ana C. Marques   +3 more
openalex   +1 more source

Investigation of in-plane wave motion in a Fibre Metal Laminate using PVDF foil sensors

, 2020
Liv Rittmeier, Tobias Losch, Michael Sinapius, Rolf Lammering   +3 more
openalex   +1 more source

Thermal Stability and Degradation Behavior of Fibre Metal Mesh Laminate Composites by Thermo Gravimetric Analysis

, 2016

openalex   +1 more source

Failure Analysis and Mechanisms of Failure of Fibrous Composite Structures [PDF]

The state of the art of failure analysis and current design practices, especially as applied to the use of fibrous composite materials in aircraft structures is discussed.
Noor, A. K., Shuart, M. J., Starnes, J. H., Jr., Williams, J. G.   +3 more
core   +1 more source

Lightweight glass veils for fibre metal laminates

Reinforced Plastics
Technical Fibre Products technology used in University of Edinburgh study.
openaire   +1 more source

Modeling fatigue crack growth in cross ply titanium matrix composites [PDF]

In this study, the fatigue crack growth behavior of fiber bridging matrix cracks in cross-ply SCS-6/Ti-15-3 and SCS-6/Timetal-21S laminates containing center holes was investigated.
Bakuckas, J. G., Jr., Johnson, W. S.
core   +1 more source