Finite Element Analysis of Aircraft Radial Engineconnecting Rod Using Composite Material
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Abstract
The main objective of this project is analysis of Aircraft radial engine connecting rod by using fiber matrix composite materials in this type of composite materials to improve their ductility properties aluminium metal powder will be added in the matrix components like epoxy resin elements from the resin considerations the metal powder will be 5-10% of the weight of aluminium powder only added, the comparison of the existing material with GFRP Reinforced aluminium powder and Pure GFRP Material from the comparison of stress, strain and deformation results from the ANSYS Software GFRP with Aluminium powder material will get best results
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