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

---
 .../Chapter04.ipynb                                | 95 ++++++++++++++++++++++
 1 file changed, 95 insertions(+)
 create mode 100755 Aircraft_Structures_for_Engineering_Students/Chapter04.ipynb

(limited to 'Aircraft_Structures_for_Engineering_Students/Chapter04.ipynb')

diff --git a/Aircraft_Structures_for_Engineering_Students/Chapter04.ipynb b/Aircraft_Structures_for_Engineering_Students/Chapter04.ipynb
new file mode 100755
index 00000000..365fa5fb
--- /dev/null
+++ b/Aircraft_Structures_for_Engineering_Students/Chapter04.ipynb
@@ -0,0 +1,95 @@
+{
+ "metadata": {
+  "name": "",
+  "signature": "sha256:6a67de7af4fe617483b9aefeefdb01f122e2016e5ab212db494104a83b9deeda"
+ },
+ "nbformat": 3,
+ "nbformat_minor": 0,
+ "worksheets": [
+  {
+   "cells": [
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 4.6 Pg.No.106"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "from __future__ import division\n",
+      "import math\n",
+      "\n",
+      "sum_FAFlBL=1263.6*10**6    # (N.mm)\n",
+      "sum_FAFlDL=880*10**6       # (N.mm)\n",
+      "E=200000                  # young's modulus (N/mm^2)\n",
+      "A=1800                    # area of each member (mm^2)\n",
+      "\n",
+      "#eqn 4.23 We=Wi\n",
+      "del_B=sum_FAFlBL/A/E\n",
+      "print \"\\ndeflection at point B =%2.2f mm\\n\"%(del_B)\n",
+      "\n",
+      "del_D=sum_FAFlDL/A/E\n",
+      "print \"deflection at point D =%2.2f mm\\n\"%(del_D)\n"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "deflection at point B =3.51 mm\n",
+        "\n",
+        "deflection at point D =2.44 mm\n",
+        "\n"
+       ]
+      }
+     ],
+     "prompt_number": 19
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "from __future__ import division\n",
+      "import math\n",
+      "\n",
+      "ext_load=30    #external load(kN)\n",
+      "\n",
+      "#eqn 30*4*del_vB/3=F_BA*del_vB\n",
+      "F_BA=ext_load*4/3\n",
+      "print \"\\nforce in the struss AB is = %3.2f kN\\n\"%(F_BA)"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "force in the struss AB is = 40.00 kN\n",
+        "\n"
+       ]
+      }
+     ],
+     "prompt_number": 18
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [],
+     "language": "python",
+     "metadata": {},
+     "outputs": []
+    }
+   ],
+   "metadata": {}
+  }
+ ]
+}
\ No newline at end of file
-- 
cgit