Abstract:

Vibration characteristics of 2124A/SiC/25P metal matrix composites and aluminum 6061-T6 materials are compared with FEA. These materials, which are widely used in the aircraft industry is different vibration characteristics. These materials are usually subjected to dynamic loadings in aerospace. Vibration analysis that is determined from stress and frequency is important vibration analysis is important. Therefore, in this study, vibration response of two different materials were examined. Vibration analysis using a distributed point and forced damped was performed in the MSC ACTRAN program. Metal matrix composites according to the aluminum alloy were found to be more stable against vibration resistance.

Keywords: