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Overview and Aim

This was done as a part of edx.com online course to gain more knowledge about Finite Element Analysis and use of ANSYS software. In this, static analysis of bike crank and a bolted flange of a rocket nozzle  is analysed in ANSYS 17 workbench

Bike crank and bolted flange Static Structural Analysis

The static analysis of the bike crank is done by size of the element as 0.2 in and the solving method is Multi zoned and then Displacement and the stress in the X-direction are calculated.

The calculated values are verified with the hand calculation

The figure on the right shows the mesh generated in ANSYS of the crank

The figure on the left shows the Displacement plot of the crank with the boundary conditions applied

The figure on the right shows the stress along X-direction plot of the crank with the boundary conditions applied

The static analysis of the nozzle is done by taking the size of the elements for the body as 0.3 in and the size of the elements for the bolt and nut as 0.075 in and the method used for solving is the Hexa Dominant

Description

Analyzing the bolted joint by non linear finite element model in ANSYS. Finding the failure criteria of the bolted flange is the main objective of this problem

The entire problem is simplified by taking only 0.9 degree  slice of the entire nozzle

The figure on the left shows the meshed part of the 0.9 degree slice of the entire nozzle

The total deformation of the entire body and the gap between the two nozzles are simulated and calculated in ANSYS, to interpret the simulated results these are compared with the hand calculations

The below figures shows the simulated results of total deformation and the gap between the bolted nozzle

Total Derformation of the entire body

Gap between the two bolted nozzle parts considering preload of bolt

Gap between the two bolted nozzle parts considering preload and pressure

Total Gap between the two bolted nozzle parts considering preload, pressure and thermal expansion

The figure on the right shows the force convergence of the ANSYS solver

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