Advanced Structural Analysis using Solidworks simulation - Stress concentration on plates with holes

  Objective: The aim of this project is to analyse the performance of three different types of beams under the same bending load, compare the results for stress, displacement and strain and choose the most efficient beam out of the three. Introduction: The beam, or flexural member, is frequently encountered in…

Title:  OBJECTIVE: The project involves performing a static structural analysis using Solidworks simulation, on two models to find out and compare the deformation and maximum stress in two plates and their behaviour around stress concentration regions like holes. INTRODUCTION: The entire process of performing a solidworks…

TITLE: Frequency analysis of a rotating shaft with a mounted circular disc using Solidworks simulation   Objective:The aim of the project is to conduct a frequency analysis on a shaft with a disc mounted on it and determine the corresponding resonant frequencies and the mode shapes. Introduction: Natural Frequency:…

BUCKLING ANALYSIS OF A CYCLONIC SEPERATOR STAND - SIMULATION & DESIGN OPTIMIZATION   OBJECTIVE: The objective of this project is to perform a buckling analysis on a cyclonic separator stand.The project involves simulation done in two cases followed by a Design optimization study of the second case.  …

Curve fitting is a powerful tool which examines the relationship between two or more variables with the goal of defining the relationship between them in the best or most accurate possible way.In other words, Curve fitting is the process of constructing a curve, or mathematicalfunction, that has the best fit to a series…

%Solving a second order linear ODE and creating a pendulum animation clear all close all clc %input values as provided b=0.05; g=9.81; l=1; m=1; %intial conditions thetha_0=[0;3]; %time points t_span=linspace(0,20,500); %the function ode_func has the ode that governs the motion of the pendulum %results is a 2 column solution…

%AIR STANDARD CYCLE (OTTO CYCLE) STATE POINTS AND PV PLOT clear all close all clc %inputs gamma = 1.4; %engine geometry bore = 0.1; stroke = 0.1; conn_rod = 0.15; cr = 12; swept_vol = (pi/4)*bore^2*stroke; clearance_vol = swept_vol/(cr-1); %state variables @ state pt 1 p1 = 101325; t1 = 300; v1 = swept_vol + clearance_vol;…