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Residual strength and sizing of aeronautical composite assemblies exposed to electric currents
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Residual strength and sizing of aeronautical composite assemblies exposed to electric currents

Type de contrat

Offre de thèse

Temps de travail

Temps plein

Diplôme

Diplôme d'ingénieur

Date limite de candidature

31/12/2025

This Cifre thesis with Airbus investigates the impact of electrical currents on composite bolted joints in CFRP airframes, aiming to understand failure mechanisms and develop predictive models for residual strength.