Results 111 to 120 of about 18,796 (217)

Modeling Composite Laminate Crushing for Crash Analysis

open access: yes, 2002
Crash modeling of composite structures remains limited in application and has not been effectively demonstrated as a predictive tool. While the global response of composite structures may be well modeled, when composite structures act as energy-absorbing
Fleming, David C., Jones, Lisa
core  

Impact on laminated composites

open access: yes, 2021
An impact is a force which is applied over a short time period. Such a force can sometimes have greater effect than a lower force applied over a proportionally longer time period. Although many structures are some time subjected to these kinds of forces, many machines and machine parts are commonly subjected to such forces.
openaire   +1 more source

Assessment of Ply Stacking Sequence Effect on Damage Behavior of CFRP Composite Laminate Under Low-Velocity Impacts

open access: yesAdvances in Materials Science and Engineering
To enhance performance under low-velocity impact (LVI), the ply stacking sequence of a composite laminate must be carefully selected. To guarantee that the laminate can sustain the projected impact energy, the impact load should be carefully evaluated ...
Murlidhar Patel   +2 more
doaj   +1 more source

Composite Laminate Delamination Detection Using Transient Thermal Conduction Profiles and Machine Learning Based Data Analysis. [PDF]

open access: yesSensors (Basel), 2020
Gillespie DI   +6 more
europepmc   +1 more source

Resin infusion of layered metal/composite hybrid and resulting metal/composite hybrid laminate

open access: yes, 2009
A method of fabricating a metal/composite hybrid laminate is provided. One or more layered arrangements are stacked on a solid base to form a layered structure. Each layered arrangement is defined by a fibrous material and a perforated metal sheet.
Weiser, Erik S.   +3 more
core  

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

open access: yes, 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
David-West, O.S.   +2 more
core  

Identification of damage in composite materials using thermoelastic stress analysis

open access: yes, 2007
A quantitative damage assessment methodology for composite materials has beenachieved using Thermoelastic Stress Analysis (TSA). The TSA technique provides fullfielddata which is collected in a non-contacting and real time manner.
Emery, Trystan Ross
core  

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