Ultrasonic fully reversed axial tests for exploring the very high cycle fatigue of composite materials

Ультразвуковые полностью реверсированные осевые испытания для изучения усталости композитных материалов в режиме очень большого числа циклов
Carlo Boursier Niutta, Andrea Tridello, Davide Salvatore Paolino
2024-10-16

Very High Cycle Fatigue (VHCF)carbon fiber twill 2x2 woven laminateembedded fiber optic temperature sensorfully reversed ultrasonic axial testhourglass specimen
• Fully reversed ultrasonic test for the VHCF response of carbon fiber woven laminate. • Strain gage calibration to exclude the presence of spurious modes. • Embedded optic fiber to measure the internal temperature increase. • Failures of hourglass specimens in the range of 10 6 -10 9 cycles and 90–155 MPa. In the present work, the feasibility of axial ultrasonic tests for exploring the fully reversed fatigue response of composite materials even in the Very High Cycle Fatigue (VHCF) regime is proved. VHCF tests are run on hourglass specimens made of twill 2x2 carbon woven fabric impregnated with epoxy resin with stacking sequences [0] 8 and [0/90/+45/-45] s and designed through Finite Element (FE) modal analysis. The stress distribution within the specimen and the absence of buckling are first determined through an extensive strain gage campaign, which has validated the FE model. As the temperature is a main concern in ultrasonic tests, the temperature increment within the composite specimen is investigated by means of an embedded fiber optic sensor and controlled during the tests with an infrared sensor. With the proposed experimental setup, fully reversed ultrasonic tests have been carried out up to 10 9 cycles and the failure of the two investigated specimen types has been analyzed by comparing the failure origin location in relation to the stress distributions.
1
Axial ultrasonic testing is feasible for fully reversed VHCF (up to 10^9 cycles) of carbon fiber woven laminate specimens.
2
Embedded fiber optic sensors measured internal temperature rise and, together with infrared monitoring, allowed temperature control during ultrasonic VHCF testing.
3
Failure origins were analyzed relative to measured stress distributions, enabling comparison between the two stacking sequences under VHCF conditions.
4
Finite Element modal analysis guided specimen design and was validated by an extensive strain gage campaign confirming stress distribution and absence of buckling.
5
Hourglass specimens of twill 2x2 carbon woven fabric (stackings [0]8 and [0/90/+45/-45]s) failed between 10^6 and 10^9 cycles at stress levels 90–155 MPa.

Hourglass composite specimens made of twill 2x2 carbon woven fabric impregnated with epoxy resin (stacking sequences [0]8 and [0/90/+45/-45]s) subjected to axial fully reversed ultrasonic fatigue testing

Very High Cycle Fatigue (VHCF) fully reversed axial fatigue response including failure cycles (10^6–10^9), failure origins/location relative to stress distribution, strain-field validation, and internal temperature increase during ultrasonic testing

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2024-10-16
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Carlo Boursier Niutta
Andrea Tridello
Davide Salvatore Paolino
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