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+{
+ "metadata": {
+  "name": "",
+  "signature": "sha256:be59baaa0b424ca36821aba74f7944f301ffd891c617783ec6544d131134dbbb"
+ },
+ "nbformat": 3,
+ "nbformat_minor": 0,
+ "worksheets": [
+  {
+   "cells": [
+    {
+     "cell_type": "heading",
+     "level": 1,
+     "metadata": {},
+     "source": [
+      "Chapter 10 : The Boundary Layer"
+     ]
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 10.1 Page No : 379"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "import math \n",
+      "\t\t\t\n",
+      "#Initialization of variables\n",
+      "v = 30.      \t\t\t#velocity - m/s\n",
+      "nu = 1.5e-5 \t\t\t#m**2/s\n",
+      "\t\t\t\n",
+      "#calculations\n",
+      "Re = 5*10**5\n",
+      "xc =  Re*nu/v\n",
+      "\t\t\t\n",
+      "#results\n",
+      "print \"Transistion region  =  %.2f m\"%(xc)"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "Transistion region  =  0.25 m\n"
+       ]
+      }
+     ],
+     "prompt_number": 1
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 10.2 Page No : 388"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "import math \n",
+      "\t\t\t\n",
+      "#Initialization of variables\n",
+      "u = 2. \t\t\t    #velocity - m/s\n",
+      "x = 0.15 \t\t\t#length - m\n",
+      "nu = 1.5e-5 \t\t#m**2/s\n",
+      "B = 0.5 \t\t\t#m\n",
+      "rho = 1.22 \t\t\t#kg/m**3\n",
+      "\n",
+      "#calcualtions\n",
+      "Rx = u*x/nu\n",
+      "delta =  4.91*x/math.sqrt(Rx)\n",
+      "deltas = 1.729*x/math.sqrt(Rx)\n",
+      "Cf = 1.328/math.sqrt(Rx)\n",
+      "Ff = Cf*0.5*rho*u**2 *2*B*x\n",
+      "\t\t\t\n",
+      "#results\n",
+      "print \"Boundary layer thickness  =  %.2f cm\"%(delta*100)\n",
+      "print \" Displacement thickness  =  %.2f cm\"%(deltas*100)\n",
+      "print \" Average drag coeffcient  =  %.4f\"%(Cf)\n",
+      "print \" Drag force  =  %.4f N\"%(Ff)"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "Boundary layer thickness  =  0.52 cm\n",
+        " Displacement thickness  =  0.18 cm\n",
+        " Average drag coeffcient  =  0.0094\n",
+        " Drag force  =  0.0034 N\n"
+       ]
+      }
+     ],
+     "prompt_number": 2
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 10.5 Page No : 400"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "import math \n",
+      "\t\t\t\n",
+      "#Initialization of variables\n",
+      "U = 172.*1000/3600 \t\t\t#m/s\n",
+      "w = 3. \t        \t\t#m\n",
+      "h = 3. \t\t        \t#m\n",
+      "L = 100. \t\t\t    #m\n",
+      "nu = 1.5e-5 \t\t\t#m**2/s\n",
+      "rho = 1.22 \t    \t\t#kg/m**3\n",
+      "\t\t\t\n",
+      "#calculations\n",
+      "Rl = U*L/nu\n",
+      "Cf = 0.074 /(Rl**(1./5))\n",
+      "Ff = Cf*0.5*rho*U**2 *w*h*L\n",
+      "power =  Ff*U\n",
+      "\t\t\t\n",
+      "#results\n",
+      "print \"power required  =  %.1f kW\"%(power/1000)\n",
+      "#The answer is a bit different due to rounding off error"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "power required  =  88.3 kW\n"
+       ]
+      }
+     ],
+     "prompt_number": 3
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 10.6 Page No : 400"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "import math \n",
+      "\t\t\t\n",
+      "#Initialization of variables\n",
+      "U = 4000. \t\t    \t#m/s\n",
+      "L = 8. \t\t        \t#m\n",
+      "nu = 3600.e-6 \t\t\t#m**2/s\n",
+      "rho = 1000. \t\t\t#kg/m**3\n",
+      "b = 5.       \t\t\t#m\n",
+      "\t\t\t\n",
+      "#calculations\n",
+      "Rl = U*L/nu\n",
+      "Cf =  0.074/Rl**(1./5) -1700/Rl\n",
+      "Ff = Cf*0.5*rho*(U/3600)**2 *L*b\n",
+      "\t\t\t\n",
+      "#results\n",
+      "print \"Skin friction drag  =  %.2f N\"%(Ff)\n",
+      "\n",
+      "# note : rounding off error."
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "Skin friction drag  =  69.75 N\n"
+       ]
+      }
+     ],
+     "prompt_number": 1
+    }
+   ],
+   "metadata": {}
+  }
+ ]
+}
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