From 92cca121f959c6616e3da431c1e2d23c4fa5e886 Mon Sep 17 00:00:00 2001
From: hardythe1
Date: Tue, 7 Apr 2015 15:58:05 +0530
Subject: added books

---
 .../Chapter08.ipynb                                | 154 +++++++++++++++++++++
 1 file changed, 154 insertions(+)
 create mode 100755 Aircraft_Structures_for_Engineering_Students/Chapter08.ipynb

(limited to 'Aircraft_Structures_for_Engineering_Students/Chapter08.ipynb')

diff --git a/Aircraft_Structures_for_Engineering_Students/Chapter08.ipynb b/Aircraft_Structures_for_Engineering_Students/Chapter08.ipynb
new file mode 100755
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--- /dev/null
+++ b/Aircraft_Structures_for_Engineering_Students/Chapter08.ipynb
@@ -0,0 +1,154 @@
+{
+ "metadata": {
+  "name": "",
+  "signature": "sha256:d4ab160ecba8745ef027bb167a7abbd97977707c483b1d0a639c7f068e2016a8"
+ },
+ "nbformat": 3,
+ "nbformat_minor": 0,
+ "worksheets": [
+  {
+   "cells": [
+    {
+     "cell_type": "heading",
+     "level": 1,
+     "metadata": {},
+     "source": [
+      "Chapter 08: Columns"
+     ]
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 8.3 Pg.No.280"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "from __future__ import division\n",
+      "import math\n",
+      "\n",
+      "E=75000         #youngs modulus(N/mm^2)\n",
+      "G=21000          #shear modulus (N/mm^2)\n",
+      "L=2              #length of column (m)\n",
+      "l1=75            #flange length (mm)\n",
+      "l2=37.5            #total length(mm)\n",
+      "t=2.5            #thickness(mm)\n",
+      "\n",
+      "A=t*(2*l2+l1)         #observed from Fig 8.17\n",
+      "\n",
+      "#chapter 16  Ixx=bd^3/12+Ab^2\n",
+      "Ixx=2*l2*t*l2**2+t*l1**3/12\n",
+      "Iyy=2*t*l2**3/12\n",
+      "\n",
+      "I0=Ixx+Iyy\n",
+      "\n",
+      "#eqn 18.11 J=SUM((s*t^3)/3)\n",
+      "J=2*l2*t**3/3+l1*t**3/3\n",
+      "\n",
+      "Gama=t*l2**3*l1**2/24\n",
+      "Iyy=0.22*10**5\n",
+      "L=2*10**3\n",
+      "P_CRxx=math.pi**2*E*Ixx/L**2\n",
+      "P_CRyy=math.pi**2*E*Iyy/L**2\n",
+      "P_CRo=A/I0*(G*J+math.pi**2*E*Gama/L**2)\n",
+      "\n",
+      "print \"P_CRxx = %3.2e N\\n\"%(P_CRxx)\n",
+      "print \"P_CRyy = %0.1e N\\n\"%(P_CRyy)\n",
+      "print \"P_CRO = %0.2e N\\n\"%(P_CRo)\n",
+      "\n",
+      "print \"therefore buckling in the column due to axial load=%0.1e N\\n\"%(P_CRyy)"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "P_CRxx = 6.51e+04 N\n",
+        "\n",
+        "P_CRyy = 4.1e+03 N\n",
+        "\n",
+        "P_CRO = 2.22e+04 N\n",
+        "\n",
+        "therefore buckling in the column due to axial load=4.1e+03 N\n",
+        "\n"
+       ]
+      }
+     ],
+     "prompt_number": 9
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 8.4 Pg.No.282"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "from __future__ import division\n",
+      "import math\n",
+      "import numpy as np\n",
+      "from sympy import solve, symbols, pprint\n",
+      "from sympy import diff\n",
+      "P=symbols('P')\n",
+      "\n",
+      "E=70000        #youngs modulus (N/mm^2)\n",
+      "G=30000         #shear modulus (N/mm^2)\n",
+      "x_S=-76.2        #position of shear center(mm)\n",
+      "l1=l2=100        #lengths (mm)\n",
+      "t=2              #thickness(mm)\n",
+      "\n",
+      "x_bar=2*t*l1*50/(3*l1)/2\n",
+      "\n",
+      "A=600         #area (mm^2)\n",
+      "Ixx=1.17*10**6    #second moment of area (mm^4)\n",
+      "Iyy=0.67*10**6    #second moment of area (mm^4)\n",
+      "I0=5.32*10**6     # total second moment of area (mm^4)\n",
+      "J=800              #torsion constant (mm^4)\n",
+      "Gama=2488*10**6     #(mm^6)\n",
+      "L=10**3             #(mm)\n",
+      "\n",
+      "P_CRxx=math.pi**2*E*Ixx/L**2\n",
+      "P_CRyy=math.pi**2*E*Iyy/L**2\n",
+      "P_CRo=A/I0*(G*J+math.pi**2*E*Gama/L**2)\n",
+      "\n",
+      "fun=P**2*(1-A*x_S**2/I0)-P*(P_CRxx+P_CRo)+P_CRxx*P_CRo\n",
+      "solution = solve(fun, P)\n",
+      "print \"lowest value of critical load = %1.2e N\\n\"%(min(solution))"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "lowest value of critical load = 1.68e+05 N\n",
+        "\n"
+       ]
+      }
+     ],
+     "prompt_number": 29
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [],
+     "language": "python",
+     "metadata": {},
+     "outputs": []
+    }
+   ],
+   "metadata": {}
+  }
+ ]
+}
\ No newline at end of file
-- 
cgit