Stresses Occurring on a Cylinder with Annular Silicon Carbide (SiC), Ti6Al4V and Copper (Cu) materials

Abstract

In this study, the stresses occurring in the annular cylinder modeled as a circular layer were analyzed numerically. Of the materials selected in accordance with the cylinder; Silicon Carbide (SiC) is known to be frequently used in the avia-tion industry due to the high abrasion and erosion resistance of the material. In this study, Silicon Carbide (SiC) is lo-cated in the upper layer of the annular cylinder due to its high strength. Titanium alloy and Ti6Al4V materials are also used in the aircraft and defense industry, where high strength, low weight and resistance to high temperatures are of great importance. Copper (Fr) material also shows high corrosion resistance. At the end of the study, it was seen that Silicon Carbide (SiC) with high elastic modulus has higher resistance to heat than Ti6Al4V (Titanium alloy) material. It has been observed that the stresses occurring in the Ti6Al4V (Titanium alloy) material part are higher than in the Cop-per (Cu) material Fractions. The results obtained at the end of the study were shared with graphs. In addition to the results obtained, the stresses obtained in a regional part of the disk with the ANSYS 2024 program were shown with graphs.

Keywords

• cylinder
• mathematical formulation
• stress analysis

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