Post-impact flexural behavior of carbon-aramid/epoxy hybrid composites

Volume: 239, Pages: 112022 - 112022
Published: May 1, 2020
Abstract
Hybrid polymeric composites are currently used in aerospace structures due to their specific strength and stiffness as well as larger design space. This paper presents an experimental study on residual flexural strength of impacted Carbon-aramid/Epoxy hybrid composite laminates. Specimens are designed in a sandwich form in which plies of aramid/epoxy represent the core and carbon/epoxy plies play the role of face sheets. This design is expected...
Paper Details
Title
Post-impact flexural behavior of carbon-aramid/epoxy hybrid composites
Published Date
May 1, 2020
Volume
239
Pages
112022 - 112022
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