6533b7d7fe1ef96bd1268f68
RESEARCH PRODUCT
Determination of the residual stresses in composite laminate using the compliance method
Guillaume MontayAbel CherouatJian LuXiaolu GongOlivier Sicotsubject
Materials science[SPI] Engineering Sciences [physics]Composite number02 engineering and technologyCompliance method[SPI]Engineering Sciences [physics]0203 mechanical engineeringResidual stress[SPI.MECA.MEMA]Engineering Sciences [physics]/Mechanics [physics.med-ph]/Mechanics of materials [physics.class-ph]General Materials ScienceComposite materialStrain gaugeGroove (music)ComputingMilieux_MISCELLANEOUSbusiness.industryMechanical EngineeringEpoxyStructural engineeringComposite laminates021001 nanoscience & nanotechnologyCondensed Matter PhysicsFinite element method020303 mechanical engineering & transportsMechanics of Materialsvisual_artvisual_art.visual_art_medium0210 nano-technologybusinessdescription
Residual stresses play an important role on the mechanical behavior of composite laminate. The development of new methods to determine the residual stresses gradient within the laminates is necessary. This article presents the adaptation of the compliance method in the case of composite laminates carbon/epoxy [02/902]s. The incremental drilling of a constant width groove allows for each increment to measure the strains (using strain gages) and displacements (using an optical device) of particularly points of the structure surface. These experimental data are compared with results given by a finite elements simulation. This comparison allows to raise the residual stresses in the composite laminate.
| year | journal | country | edition | language |
|---|---|---|---|---|
| 2005-07-01 |