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+{
+ "cells": [
+ {
+ "cell_type": "markdown",
+ "metadata": {},
+ "source": [
+ "# Chapter 4 Centroid Centre of mass and Centre of Gravity"
+ ]
+ },
+ {
+ "cell_type": "markdown",
+ "metadata": {},
+ "source": [
+ "# Example 4.8 Centroid of a composite plane figure"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "execution_count": 1,
+ "metadata": {
+ "collapsed": false
+ },
+ "outputs": [
+ {
+ "name": "stdout",
+ "output_type": "stream",
+ "text": [
+ "The centroid of the un equal I-section is 10.961538 cm \n",
+ "\n"
+ ]
+ }
+ ],
+ "source": [
+ "# Initilization of variables\n",
+ "b1=20 #cm # width of top flange\n",
+ "t1=5 #cm # thickness of top flange\n",
+ "b2=5 #cm # width of web\n",
+ "t2=15 #cm # thickness or height of the web\n",
+ "b3=30 #cm # width of bottom flange\n",
+ "t3=5 #cm # thickness of bottom flange\n",
+ "# Calculations\n",
+ "A1=b1*t1 #cm**2 # area of bottom flange\n",
+ "A2=b2*t2 #cm**2 # area of the web\n",
+ "A3=b3*t3 #cm**2 # area of top flange\n",
+ "y1=t3+t2+(t1/2) #cm # y co-ordinate of the centroid of top flange\n",
+ "y2=t3+(t2/2) #cm # y co-ordinate of the centroid of the web\n",
+ "y3=t3/2 #cm # y co-ordinate of the centroid of the bottom flange\n",
+ "y_c=((A1*y1)+(A2*y2)+(A3*y3))/(A1+A2+A3) #cm # where y_c is the centroid of the un-symmetrical I-section\n",
+ "# Results\n",
+ "print('The centroid of the un equal I-section is %f cm \\n'%y_c)"
+ ]
+ },
+ {
+ "cell_type": "markdown",
+ "metadata": {},
+ "source": [
+ "# Example 4.9 Centroid of a composite plane figure"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "execution_count": 2,
+ "metadata": {
+ "collapsed": false
+ },
+ "outputs": [
+ {
+ "name": "stdout",
+ "output_type": "stream",
+ "text": [
+ "The centroid of the cross-sectional area of a Z-section about x-axis is 13.557692 cm \n",
+ "\n",
+ "The centroid of the cross-sectional area of a Z-section about y-axis is 7.692308 cm \n",
+ "\n"
+ ]
+ }
+ ],
+ "source": [
+ "# Initilization of variables\n",
+ "# The given section is Z-section which is un-symmetrycal about both the axis\n",
+ "b1=20 #cm # width of bottom flange \n",
+ "t1=5 #cm # thickness of the bottom flange\n",
+ "b2=2.5 #cm # thickness of the web of the flange\n",
+ "t2=15 #cm # depth of the web\n",
+ "b3=10 #cm # width of the top flange\n",
+ "t3=2.5 #cm # thickness of the top flange\n",
+ "# Calculations\n",
+ "# Respective areas\n",
+ "A1=b1*t1 # cm**2 # area of the bottom flange\n",
+ "A2=b2*t2 # cm**2 # area of the web\n",
+ "A3=b3*t3 # cm**2 # area of the top-flange\n",
+ "# first we calculate the x co-ordinate of the centroid\n",
+ "x1=b3-b2+(b1/2) #cm # for the bottom flange\n",
+ "x2=b3-(b2/2) #cm # for the web\n",
+ "x3=b3/2 #cm # for the top flange\n",
+ "x_c=((A1*x1)+(A2*x2)+(A3*x3))/(A1+A2+A3) #cm\n",
+ "# secondly we calculate the y co-ordinate of the centroid\n",
+ "y1=t1/2 #cm # for the bottom flange\n",
+ "y2=t1+(t2/2) #cm # for the web\n",
+ "y3=t1+t2+(t3/2) #cm # for the top flange\n",
+ "y_c=((A1*y1)+(A2*y2)+(A3*y3))/(A1+A2+A3) # cm\n",
+ "# Results\n",
+ "print('The centroid of the cross-sectional area of a Z-section about x-axis is %f cm \\n'%x_c)\n",
+ "print('The centroid of the cross-sectional area of a Z-section about y-axis is %f cm \\n'%y_c)"
+ ]
+ }
+ ],
+ "metadata": {
+ "kernelspec": {
+ "display_name": "Python 3",
+ "language": "python",
+ "name": "python3"
+ },
+ "language_info": {
+ "codemirror_mode": {
+ "name": "ipython",
+ "version": 3
+ },
+ "file_extension": ".py",
+ "mimetype": "text/x-python",
+ "name": "python",
+ "nbconvert_exporter": "python",
+ "pygments_lexer": "ipython3",
+ "version": "3.5.1"
+ },
+ "widgets": {
+ "state": {},
+ "version": "1.1.2"
+ }
+ },
+ "nbformat": 4,
+ "nbformat_minor": 0
+}