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Diffstat (limited to 'Advanced_Strength_and_Applied_Elasticity/Chapter11.ipynb')
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diff --git a/Advanced_Strength_and_Applied_Elasticity/Chapter11.ipynb b/Advanced_Strength_and_Applied_Elasticity/Chapter11.ipynb new file mode 100755 index 00000000..ba80b825 --- /dev/null +++ b/Advanced_Strength_and_Applied_Elasticity/Chapter11.ipynb @@ -0,0 +1,82 @@ +{
+ "metadata": {
+ "name": "",
+ "signature": "sha256:f729277270c4906babbae57b26d0a48c913109394e1fe2bf1cae355bbbb10bbd"
+ },
+ "nbformat": 3,
+ "nbformat_minor": 0,
+ "worksheets": [
+ {
+ "cells": [
+ {
+ "cell_type": "heading",
+ "level": 1,
+ "metadata": {},
+ "source": [
+ "Chapter11-Elastic Stability"
+ ]
+ },
+ {
+ "cell_type": "heading",
+ "level": 2,
+ "metadata": {},
+ "source": [
+ "Ex1-pg319"
+ ]
+ },
+ {
+ "cell_type": "code",
+ "collapsed": false,
+ "input": [
+ "import math\n",
+ "#calcualte weight and N\n",
+ "E=210*10**9. ##Pa\n",
+ "d=100. ##mm\n",
+ "t=50 ##mm\n",
+ "A=0.005\n",
+ "Iz=0.05*(0.1**3)/12.\n",
+ "print(Iz)\n",
+ "Iy=0.1*(0.05**3)/12\n",
+ "print(Iy)\n",
+ "##r=sqrt(Iy/A)\n",
+ "r= math.sqrt(Iy/A)\n",
+ "print(r)##mm\n",
+ "L=2.75\n",
+ "\n",
+ "##P=W/tand(15)=3.732\n",
+ "Pcr=(math.pi**2.*E*Iz)/L**2.\n",
+ "print'%s %.2f %s'%(\"into W is= \",Pcr,\"\")\n",
+ "W=Pcr/3.732\n",
+ "print'%s %.2f %s'%(\"in N is= \",W,\"\")\n",
+ "\n",
+ "Pcr=(math.pi**2*E*Iy)/L**2.\n",
+ "print'%s %.2f %s'%(\"into W is= \",Pcr,\"\")\n",
+ "W=Pcr/3.732\n",
+ "print'%s %.2f %s'%(\"in N is= \",W,\"\")\n",
+ "\n",
+ "## Ans varies due to round of error\n"
+ ],
+ "language": "python",
+ "metadata": {},
+ "outputs": [
+ {
+ "output_type": "stream",
+ "stream": "stdout",
+ "text": [
+ "4.16666666667e-06\n",
+ "1.04166666667e-06\n",
+ "0.0144337567297\n",
+ "into W is= 1141937.70 \n",
+ "in N is= 305985.45 \n",
+ "into W is= 285484.42 \n",
+ "in N is= 76496.36 \n"
+ ]
+ }
+ ],
+ "prompt_number": 1
+ }
+ ],
+ "metadata": {}
+ }
+ ]
+}
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