Results 21 to 30 of about 215,695 (266)

A simulative study on the effect of friction coefficient and angle on failure behaviors of GLARE subjected to low-velocity impact

open access: yesScience and Engineering of Composite Materials, 2023
The aim of this paper is to study the effect of friction coefficient and impact angle on the failure behaviors of glass fiber reinforced aluminum laminates (GLARE) under the low-velocity impact (LVI) loading.
You Peiyu, Chen Hui, Li Mingjie, Wu Ye
doaj   +1 more source

Delamination Effect on the Buckling Behaviour of Carbon–Epoxy Composite Typical Aeronautical Panels

open access: yesApplied Sciences, 2023
The instability of structures due to compression is one of the most critical issues related to aircraft components. Especially in composite materials, which have poor out-of-plane mechanical properties, the buckling load must be assessed to ensure that ...
Aniello Riccio   +3 more
doaj   +1 more source

Validation of low velocity impact modelling on different stacking sequences of CFRP laminates and influence of fibre failure [PDF]

open access: yes, 2013
This paper presents a validation of low-velocity impact Finite Element (FE) modelling. Based on switching ply location of reference layup [02,452,902,-452]s T700GC/M21 laminated plates from Bouvet et al.
Bouvet, Christophe   +2 more
core   +1 more source

Post-Impact Compression Behavior of Natural Flax Fiber Composites

open access: yesJournal of Natural Fibers, 2020
This study investigated the damage tolerance and damage evolution of the compressive failure of a non-woven flax composite using compression after impact (CAI) tests.
Mohamed Habibi   +4 more
doaj   +1 more source

Impact-induced bonding process of copper at low velocity and room temperature

open access: yesMaterials & Design, 2023
The impact-induced bonding can be foundation of fast solid-state additive manufacturing. The mechanisms behind impact-induced bonding have not been widely acknowledged due to complexity caused by too transient process and extreme loading conditions.
Cong Chen   +8 more
doaj   +1 more source

Impact behaviour of an innovative trapezoidal composite corrugated core sandwich structure under low-velocity impact: an experimental and numerical study [PDF]

open access: yes, 2020
Composite core sandwich structures have been extensively used in aerospace, marine and automotive applications. A few configurations of composite cores have been used in manufacturing sandwich structures for many years.
Zangana, Sartip
core   +1 more source

Improvement of low-velocity impact and compression-after-impact performance by z-fibre pinning. [PDF]

open access: yes, 2006
Z-fibre® pinning is a new method of through-thickness reinforcement of laminated composites. This paper presents an experimental test and theoretical analysis on how and why these pins can improve the resistance to impact loading and post- impact ...
X. Zhang   +5 more
core   +1 more source

Low velocity impact response and post impact compression behavior of BMI matrix composites

open access: yesCailiao gongcheng, 2022
A novel kind of lattice-distributed ESTM-fabrics was developed by using polyethersulfone(PES) and U3160.The loading amounts of PES on ESTM-fabrics are 15 g/cm2(ES-15), 25 g/cm2(ES-25), 35 g/cm2(ES-35), respectively.
DONG Huimin   +4 more
doaj   +1 more source

Velocity equation for grenades while impacting on dry sand media

open access: yesDefence Technology
This paper deals with the collision of sphere shape grenades with sand media. The central issue of the article is the establishing of an empirical velocity equation of the grenade while impacting on sand that is used to solve motion equations of the ...
Martin Macko   +6 more
doaj   +1 more source

Palliatives for Low Velocity Impact Damage in Composite Laminates

open access: yesAdvances in Materials Science and Engineering, 2017
Fibre reinforced polymer laminated composites are susceptible to impact damage during manufacture, normal operation, maintenance, and/or other stages of their life cycle.
Mubarak Ali   +2 more
doaj   +1 more source

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