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+{
+ "metadata": {
+  "name": ""
+ },
+ "nbformat": 3,
+ "nbformat_minor": 0,
+ "worksheets": [
+  {
+   "cells": [
+    {
+     "cell_type": "heading",
+     "level": 1,
+     "metadata": {},
+     "source": [
+      "One-dimensional, Steady State Conduction"
+     ]
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.1 Page 104"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "\n",
+      "# Find Skin Temperature & Aerogel Insulation Thickness \n",
+      "import math\n",
+      "A=1.8;    \t\t\t\t\t# [m^2] Area for Heat transfer i.e. both surfaces\n",
+      "Ti = 35+273.;  \t\t\t\t#[K] - Inside Surface Temperature of Body\n",
+      "Tsurr = 10+273.; \t\t\t#[K] - Temperature of surrounding\n",
+      "Tf = 283.; \t\t\t\t\t#[K] - Temperature of Fluid Flow\n",
+      "e=.95; \t\t\t\t\t\t#  Emissivity of Surface\n",
+      "Lst=.003;    \t\t\t\t#[m] - Thickness of Skin\n",
+      "kst=.3; \t\t \t\t\t#  [W/m.K] Effective Thermal Conductivity of Body\n",
+      "kins = .014;  \t\t\t\t#  [W/m.K] Effective Thermal Conductivity of Aerogel Insulation\n",
+      "hr = 5.9;    \t\t\t\t#[W/m^2.k] - Natural Thermal Convectivity from body to air\n",
+      "stfncnstt=5.67*math.pow(10,(-8)); # [W/m^2.K^4] - Stefan Boltzmann Constant \n",
+      "q = 100;          \t\t\t#[W] Given Heat rate\n",
+      "#calculations\n",
+      "\n",
+      "#Using Conducion Basic Eq 3.19\n",
+      "Rtot = (Ti-Tsurr)/q;\n",
+      "#Also\n",
+      "#Rtot=Lst/(kst*A) + Lins/(kins*A)+(h*A + hr*A)^-1\n",
+      "#Rtot = 1/A*(Lst/kst + Lins/kins +(1/(h+hr)))\n",
+      "\n",
+      "#Thus\n",
+      "#For Air,\n",
+      "h=2.;    \t\t\t\t\t#[W/m^2.k] - Natural Thermal Convectivity from body to air\n",
+      "Lins1 =  kins * (A*Rtot - Lst/kst - 1/(h+hr));\n",
+      "\n",
+      "#For Water,\n",
+      "h=200.;    \t\t\t\t\t#[W/m^2.k] - Natural Thermal Convectivity from body to air\n",
+      "Lins2 =  kins * (A*Rtot - Lst/kst - 1/(h+hr));\n",
+      "\n",
+      "Tsa=305.;            \t\t#[K]  Body Temperature Assumed\n",
+      "\n",
+      "#Temperature of Skin is same in both cases as Heat Rate is same\n",
+      "#q=(kst*A*(Ti-Ts))/Lst\n",
+      "Ts = Ti - q*Lst/(kst*A);\n",
+      "#results\n",
+      "\n",
+      "#Also from eqn of effective resistance Rtot F\n",
+      "print '%s %.1f %s' %(\"\\n\\n (I) In presence of Air, Insulation Thickness = \",Lins1*1000,\" mm\")\n",
+      "print '%s %.1f %s' %(\"\\n (II) In presence of Water, Insulation Thickness =\",Lins2*1000.,\" mm\");\n",
+      "print '%s %.2f %s' %(\"\\n\\n  Temperature of Skin =\",Ts-273,\" degC\");\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        " (I) In presence of Air, Insulation Thickness =  4.4  mm\n",
+        "\n",
+        " (II) In presence of Water, Insulation Thickness = 6.1  mm\n",
+        "\n",
+        "\n",
+        "  Temperature of Skin = 34.44  degC\n"
+       ]
+      }
+     ],
+     "prompt_number": 1
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.2 Page 107"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "\n",
+      "# Chip Operating Temperature\n",
+      "import math\n",
+      "Tf = 25+273.; \t\t\t#[K] - Temperature of Fluid Flow\n",
+      "L=.008;    \t\t\t\t#[m] - Thickness of Aluminium \n",
+      "k=239;  \t\t\t\t#  [W/m.K] Effective Thermal Conductivity of Aluminium\n",
+      "Rc=.9*math.pow(10,-4);  #[K.m^2/W]    Maximum permeasible Resistane of Epoxy Joint\n",
+      "q=10000.;    \t\t\t#[W/m^2]    Heat dissipated by Chip\n",
+      "h=100.;    \t\t\t\t#[W/m^2.k] - Thermal Convectivity from chip to air\n",
+      "#calculations\n",
+      "\n",
+      "#Temperature of Chip\n",
+      "\n",
+      "Tc = Tf + q/(h+1/(Rc+(L/k)+(1/h)));\n",
+      "q=(Tc-Tf)/(1/h)+(Tc-Tf)/(Rc+(L/k)+(1/h))\n",
+      "#results\n",
+      "\n",
+      "print '%s %.2f %s' %(\"\\n\\n Temperature of Chip =\",Tc-273,\"degC\");\n",
+      "print '%s' %(\"\\n Chip will Work well below its maximum allowable Temperature ie 85 degC\")\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        " Temperature of Chip = 75.31 degC\n",
+        "\n",
+        " Chip will Work well below its maximum allowable Temperature ie 85 degC\n"
+       ]
+      }
+     ],
+     "prompt_number": 2
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.3 Page 109"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "\n",
+      "# Find Thermal conductivity of Carbon Nanotube\n",
+      "import math\n",
+      "D = 14 * math.pow(10,-9);    \t\t\t# [m]Dia of Nanotube\n",
+      "s = 5*math.pow(10,-6);       \t\t\t# [m]Distance between the islands\n",
+      "Ts = 308.4;        \t\t\t\t\t\t#[K] Temp of sensing island\n",
+      "Tsurr = 300;       \t\t\t\t\t\t#[K] Temp of surrounding\n",
+      "q = 11.3*math.pow(10,-6);    \t\t\t#[W] Total Rate of Heat flow\n",
+      "\n",
+      "#Dimension of platinum line\n",
+      "wpt =math.pow(10,-6);       \t\t\t#[m]\n",
+      "tpt = 0.2*math.pow(10,-6);   \t\t\t#[m] \n",
+      "Lpt = 250*math.pow(10,-6);   \t\t\t#[m] \n",
+      "#Dimension of Silicon nitride line\n",
+      "wsn = 3*math.pow(10,-6);       \t\t\t#[m]\n",
+      "tsn = 0.5*math.pow(10,-6);  \t \t\t#[m] \n",
+      "Lsn = 250*math.pow(10,-6);   \t\t\t#[m] \n",
+      "#From Table A.1 Platinum Temp Assumed = 325K\n",
+      "kpt = 71.6;    \t\t\t\t\t\t\t#[W/m.K]\n",
+      "#From Table A.2, Silicon Nitride Temp Assumed = 325K\n",
+      "ksn = 15.5;   \t \t\t\t\t\t\t#[W/m.K]\n",
+      "#calculations\n",
+      "\n",
+      "Apt = wpt*tpt;        \t\t\t\t\t#Cross sectional area of platinum support beam\n",
+      "Asn = wsn*tsn-Apt;    \t\t\t\t\t#Cross sectional area of Silicon Nitride support beam\n",
+      "Acn = math.pi*D*D/4.;       \t\t\t#Cross sectional Area of Carbon nanotube\n",
+      "\n",
+      "Rtsupp = 1/(kpt*Apt/Lpt + ksn*Asn/Lsn); #[K/W] Thermal Resistance of each support\n",
+      "\n",
+      "qs = 2*(Ts-Tsurr)/Rtsupp;    \t\t\t#[W] Heat loss through sensing island support\n",
+      "qh = q - qs;    \t\t\t\t\t\t#[W] Heat loss through heating island support\n",
+      "\n",
+      "Th = Tsurr + qh*Rtsupp/2.;    \t\t\t#[K] Temp of Heating island\n",
+      "\n",
+      "#For portion Through Carbon Nanotube\n",
+      "\n",
+      "\n",
+      "kcn = qs*s/(Acn*(Th-Ts));\n",
+      "qs = (Th-Ts)/(s/(kcn*Acn));\n",
+      "#results\n",
+      "\n",
+      "print '%s %.2f %s' %(\"\\n\\n Thermal Conductivity of Carbon nanotube =\",kcn,\"W/m.K\");\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        " Thermal Conductivity of Carbon nanotube = 3111.86 W/m.K\n"
+       ]
+      }
+     ],
+     "prompt_number": 3
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.4 Page 113"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "\n",
+      "# Temperature Distribution And Heat rate\n",
+      "import math\n",
+      "import numpy\n",
+      "from numpy import linspace\n",
+      "import matplotlib\n",
+      "from matplotlib import pyplot\n",
+      "a = 0.25;\n",
+      "x1 = .05;      #[m] Distance of smaller end\n",
+      "x2 = .25;      #[m] Distance of larger end\n",
+      "T1 = 400;      #[K] Temperature of smaller end\n",
+      "T2 = 600;      #[K] Temperature of larger end\n",
+      "k = 3.46;      #[W/m.K] From Table A.2, Pyroceram at Temp 285K\n",
+      "T=numpy.zeros(100)\n",
+      "#calculations\n",
+      "\n",
+      "x = numpy.linspace(0.05,100,num=100);\n",
+      "i=1;\n",
+      "for i in range (0,99):\n",
+      "    z=float(x[i]);\n",
+      "    T[i]=(T1 + (T1-T2)*((1/z - 1/x1)/(1/x1 - 1/x2)));\t\n",
+      "\n",
+      "pyplot.plot(x,T);\n",
+      "pyplot.xlabel(\"x (m)\");\n",
+      "pyplot.ylabel(\"T (K)\");\n",
+      "pyplot.show()\n",
+      "qx = math.pi*a*a*k*(T1-T2)/(4*(1/x1 - 1/x2));            #[W]\n",
+      "#results\n",
+      "\n",
+      "print '%s %.2f %s' %(\"\\n\\n Heat Transfer rate =\",qx,\" W\");\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        " Heat Transfer rate = -2.12  W\n"
+       ]
+      }
+     ],
+     "prompt_number": 10
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.5 Page 119 "
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "%pylab inline\n",
+      "# Critical Thickness\n",
+      "import math\n",
+      "import numpy\n",
+      "from numpy import linspace\n",
+      "import matplotlib\n",
+      "from matplotlib import pyplot\n",
+      "k = .055;    \t\t\t\t#[W/m.K] From Table A.3, Cellular glass at Temp 285K\n",
+      "h = 5;       \t\t\t\t#[W/m^2.K]\n",
+      "ri = 5*math.pow(10,-3);     #[m]  radius of tube\n",
+      "#calculations\n",
+      "\n",
+      "rct = k/h;     \t\t\t\t# [m] Critical Thickness of Insulation for maximum Heat loss or minimum resistance\n",
+      "\n",
+      "x = numpy.linspace(0,100,num=99);\n",
+      "ycond= numpy.zeros(99);\n",
+      "yconv= numpy.zeros(99);\n",
+      "ytot= numpy.zeros(99);\n",
+      "for i in range (0,99):\n",
+      "    z=float(x[i]);\n",
+      "    ycond[i]=(2.30*math.log10((z+ri)/ri)/(2*math.pi*k));\n",
+      "    yconv[i]=1/(2*math.pi*(z+ri)*h);\n",
+      "    ytot[i]=yconv[i]+ycond[i];\n",
+      "\n",
+      "    \n",
+      "pyplot.plot(x,ytot);\n",
+      "pyplot.xlabel(\"r-ri (m)\");\n",
+      "pyplot.ylabel(\"R (m.K/W)\");\n",
+      "pyplot.show();\n",
+      "#results\n",
+      "\n",
+      "print '%s %.3f %s' %(\"\\n\\n Critical Radius is =\",rct,\"  m \")\n",
+      "print '%s %.3f %s' %(\"\\n Heat transfer will increase with the addition of insulation up to a thickness of\",rct-ri,\" m\");\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "Populating the interactive namespace from numpy and matplotlib\n"
+       ]
+      },
+      {
+       "metadata": {},
+       "output_type": "display_data",
+       "png": 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hl9uiXnPrnp+fD09PT+v7WtOf6ioQDAaD1iXoQmlpKeLi4pCUlARnZ2ety9HE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\nREQAgP8HciaKFosIw6gAAAAASUVORK5CYII=\n",
+       "text": [
+        "<matplotlib.figure.Figure at 0x42e6390>"
+       ]
+      },
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        " Critical Radius is = 0.011   m \n",
+        "\n",
+        " Heat transfer will increase with the addition of insulation up to a thickness of 0.006  m\n"
+       ]
+      }
+     ],
+     "prompt_number": 2
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.6 Page 122"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "\n",
+      "# Heat conduction through Spherical Container \n",
+      "import math\n",
+      "k = .0017;    \t\t\t\t\t\t#[W/m.K] From Table A.3, Silica Powder at Temp 300K\n",
+      "h = 5;       \t\t\t\t\t\t#[W/m^2.K]\n",
+      "r1 = 25./100.;      \t\t\t\t#[m]  Radius of sphere\n",
+      "r2 = .275;          \t\t\t\t#[m]  Radius including Insulation thickness\n",
+      "\n",
+      "#Liquid Nitrogen Properties\n",
+      "T = 77;        \t\t\t\t\t\t#[K] Temperature\n",
+      "rho = 804;     \t\t\t\t\t\t#[kg/m^3] Density\n",
+      "hfg = 2*100000.;  \t\t\t\t\t#[J/kg] latent heat of vaporisation\n",
+      "\n",
+      "#Air Properties\n",
+      "Tsurr = 300;   \t\t\t\t\t\t#[K] Temperature\n",
+      "h = 20        \t\t\t\t\t\t;#[W/m^2.K]  convection coefficient\n",
+      "#calculations\n",
+      "\n",
+      "Rcond = (1/r1-1/r2)/(4*math.pi*k);  #Using Eq 3.36\n",
+      "Rconv = 1/(h*4*math.pi*r2*r2);\n",
+      "q = (Tsurr-T)/(Rcond+Rconv);\n",
+      "\n",
+      "print '%s %.2f %s' %(\"\\n\\n (a)Rate of Heat transfer to Liquid Nitrogen\",q,\" W\");\n",
+      "\n",
+      "#Using Energy Balance q - m*hfg = 0\n",
+      "m=q/hfg;    \t\t\t\t\t\t#[kg/s] mass of nirtogen lost per second\n",
+      "mc = m/rho*3600*24*1000.;\n",
+      "#results\n",
+      "\n",
+      "print '%s %.2f %s' %(\"\\n\\n (b)Mass rate of nitrogen boil off \",mc,\"Litres/day\");\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        " (a)Rate of Heat transfer to Liquid Nitrogen 13.06  W\n",
+        "\n",
+        "\n",
+        " (b)Mass rate of nitrogen boil off  7.02 Litres/day\n"
+       ]
+      }
+     ],
+     "prompt_number": 18
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.7 Page 129"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "\n",
+      "# Composite Plane wall\n",
+      "import math\n",
+      "\n",
+      "Tsurr = 30+273.;   \t\t\t\t\t\t#[K] Temperature of surrounding Water\n",
+      "h = 1000.;     \t\t\t\t\t\t\t#[W/m^2.K] Heat Convection Coeff of Water\n",
+      "kb = 150.;    \t\t\t\t\t\t\t#[W/m.K] Material B\n",
+      "Lb = .02;    \t\t\t\t\t\t\t#[m] Thickness Material B\n",
+      "ka = 75.;    \t\t\t\t\t\t\t#[W/m.K] Material A\n",
+      "La = .05;    \t\t\t\t\t\t\t#[m] Thickness Material A\n",
+      "qa = 1.5*math.pow(10,6);\t\t\t\t#[W/m^3] Heat generation at wall A\n",
+      "qb = 0;  \t\t\t\t\t\t\t\t#[W/m^3] Heat generation at wall B\n",
+      "#calculations\n",
+      "T2 = Tsurr + qa*La/h;\n",
+      "To = 100+273.15;    \t\t\t\t    #[K] Temp of opposite end of rod\n",
+      "Rcondb = Lb/kb;\n",
+      "Rconv = 1/h;\n",
+      "T1 = Tsurr +(Rcondb + Rconv)*(qa*La);\n",
+      "#From Eqn 3.43\n",
+      "T0 = qa*La*La/(2*ka) + T1;\n",
+      "\n",
+      "#results\n",
+      "\n",
+      "print '%s %d %s' %(\"\\n\\n (a) Inner Temperature of Composite To = \",T0-273,\" degC\") \n",
+      "print '%s %d %s' %(\"\\n (b) Outer Temperature of the Composite T2 =\",T2-273,\" degC\");\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        " (a) Inner Temperature of Composite To =  140  degC\n",
+        "\n",
+        " (b) Outer Temperature of the Composite T2 = 105  degC\n"
+       ]
+      }
+     ],
+     "prompt_number": 5
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.9 Page 145 "
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "%pylab inline\n",
+      "# Heat conduction through Rod\n",
+      "import math\n",
+      "import numpy\n",
+      "from numpy import linalg\n",
+      "import matplotlib\n",
+      "from matplotlib import pyplot\n",
+      "%pylab inline\n",
+      "kc = 398.;    \t\t\t\t\t\t#[W/m.K] From Table A.1, Copper at Temp 335K\n",
+      "kal = 180.;   \t \t\t\t\t\t#[W/m.K] From Table A.1, Aluminium at Temp 335K\n",
+      "kst = 14.;    \t\t\t\t\t\t#[W/m.K] From Table A.1, Stainless Steel at Temp 335K\n",
+      "h = 100.;      \t\t\t\t\t\t#[W/m^2.K] Heat Convection Coeff of Air\n",
+      "Tsurr = 25+273.;    \t\t\t\t#[K] Temperature of surrounding Air\n",
+      "D = 5/1000.;    \t\t\t\t\t#[m] Dia of rod\n",
+      "To = 100+273.15;    \t\t\t\t#[K] Temp of opposite end of rod\n",
+      "#calculations\n",
+      "\n",
+      "#For infintely long fin m = h*P/(k*A)\n",
+      "mc = math.pow((4*h/(kc*D)),.5);\n",
+      "mal = math.pow((4*h/(kal*D)),.5);\n",
+      "mst = math.pow((4*h/(kst*D)),.5);\n",
+      "x = numpy.linspace(0,0.3,100);\n",
+      "Tc= numpy.zeros(100);\n",
+      "Tal= numpy.zeros(100);\n",
+      "Tst= numpy.zeros(100);\n",
+      "for i in range (0,100):\n",
+      "    z=x[i];\n",
+      "    Tc[i] =Tsurr + (To - Tsurr)*math.pow(2.73,(-mc*z)) - 273;\n",
+      "    Tal[i] = Tsurr + (To - Tsurr)*math.pow(2.73,(-mal*z)) -273;\n",
+      "    Tst[i] = Tsurr + (To - Tsurr)*math.pow(2.73,(-mst*z)) -273;\n",
+      "\n",
+      "\n",
+      "pyplot.plot(x,Tc,label=\"Cu\");\n",
+      "pyplot.plot(x,Tal,label=\"2024 Al\");\n",
+      "pyplot.plot(x,Tst,label=\"316 SS\");\n",
+      "pyplot.legend();\n",
+      "pyplot.xlabel(\"x (m)\");\n",
+      "pyplot.ylabel(\"T (C)\");\n",
+      "pyplot.show();\n",
+      "\n",
+      "#Using eqn 3.80\n",
+      "qfc = math.pow((h*math.pi*D*kc*math.pi/4*D*D),.5)*(To-Tsurr);\n",
+      "qfal = math.pow((h*math.pi*D*kal*math.pi/4*D*D),.5)*(To-Tsurr);\n",
+      "qfst = math.pow((h*math.pi*D*kst*math.pi/4*D*D),.5)*(To-Tsurr);\n",
+      "\n",
+      "print '%s %.2f %s %.2f %s %.2f %s' %(\"\\n\\n (a) Heat rate \\n        For Copper = \",qfc,\"W \\n        For Aluminium =\",qfal,\" W \\n        For Stainless steel = \",qfst,\" W\");\n",
+      "\n",
+      "#Using eqn 3.76 for satisfactory approx\n",
+      "Linfc = 2.65/mc;\n",
+      "Linfal = 2.65/mal;\n",
+      "Linfst = 2.65/mst;\n",
+      "\n",
+      "print '%s %.2f %s %.2f %s %.2f %s' %(\"\\n\\n (a) Rods may be assumed to be infinite Long if it is greater than equal to \\n For Copper =\",Linfc,\"m \\n        For Aluminium = \",Linfal,\" m \\n        For Stainless steel =\",Linfst,\"m\");\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "Populating the interactive namespace from numpy and matplotlib\n",
+        "Populating the interactive namespace from numpy and matplotlib\n"
+       ]
+      },
+      {
+       "metadata": {},
+       "output_type": "display_data",
+       "png": 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tYeyPYzn13CkaNmhY7eM3bIApU+CPP9QR1YUQwhD0mizS0tKKe1dXpCr76FKV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\njYULIdO4T82EELcxSrKIj48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mgQ2NrRpjbWld70o8hYVqBX5ampp80tNvJZGizxkZFS+Z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\nrkJggg==\n",
+       "text": [
+        "<matplotlib.figure.Figure at 0x43e7f50>"
+       ]
+      },
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        " (a) Heat rate \n",
+        "        For Copper =  8.33 W \n",
+        "        For Aluminium = 5.60  W \n",
+        "        For Stainless steel =  1.56  W\n",
+        "\n",
+        "\n",
+        " (a) Rods may be assumed to be infinite Long if it is greater than equal to \n",
+        " For Copper = 0.19 m \n",
+        "        For Aluminium =  0.13  m \n",
+        "        For Stainless steel = 0.04 m\n"
+       ]
+      }
+     ],
+     "prompt_number": 3
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.10 Page 156"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "\n",
+      "# Study of motorcycle finned cylinder\n",
+      "import math\n",
+      "H = .15;   \t\t\t\t\t\t#[m] height\n",
+      "k = 186;    \t\t\t\t\t#[W/m.K] alumunium at 400K\n",
+      "h = 50;      \t\t\t\t\t#[W/m^2.K] Heat convection coefficient\n",
+      "Tsurr = 300;    \t\t\t\t#[K] Temperature of surrounding air\n",
+      "To = 500;    \t\t\t\t\t#[K] Temp inside\n",
+      "\n",
+      "#Dimensions of Fin\n",
+      "N = 5;\n",
+      "t = .006;    \t\t\t\t\t#[m] Thickness\n",
+      "L = .020;     \t\t\t\t\t#[m] Length\n",
+      "r2c = .048;        \t\t\t\t#[m]\n",
+      "r1 = .025;           \t\t\t#[m]\n",
+      "#calculations\n",
+      "\n",
+      "Af = 2*math.pi*(r2c*r2c-r1*r1);\n",
+      "At = N*Af + 2*math.pi*r1*(H-N*t);\n",
+      "\n",
+      "#Using fig 3.19 \n",
+      "nf = .95;\n",
+      "\n",
+      "qt = h*At*(1-N*Af*(1-nf)/At)*(To-Tsurr);\n",
+      "qwo = h*(2*math.pi*r1*H)*(To-Tsurr);\n",
+      "#results\n",
+      "\n",
+      "print '%s %.2f %s' %(\"\\n\\n  Heat Transfer Rate with the fins =\",qt,\"W \")\n",
+      "print '%s %.2f %s' %(\" \\n  Heat Transfer Rate without the fins =\",qwo,\"W\")\n",
+      "print '%s %.2f %s' %(\"\\n Thus Increase in Heat transfer rate of\",qt-qwo,\" W is observed with fins\");\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        "  Heat Transfer Rate with the fins = 689.60 W \n",
+        " \n",
+        "  Heat Transfer Rate without the fins = 235.62 W\n",
+        "\n",
+        " Thus Increase in Heat transfer rate of 453.98  W is observed with fins\n"
+       ]
+      }
+     ],
+     "prompt_number": 21
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.11 Page 158"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "\n",
+      "# Study of Fuel-cell fan system\n",
+      "import math\n",
+      "Wc =.05;    \t\t\t\t#[m] width\n",
+      "H = .026;  \t \t\t\t\t#[m] height\n",
+      "tc = .006;  \t\t\t\t#[m] thickness of cell\n",
+      "V = 9.4;    \t\t\t\t#[m/sec] vel of cooling air\n",
+      "P = 9;      \t\t\t\t#[W] Power generated\n",
+      "C = 1000;    \t\t\t\t#[W/(m^3/s)] Ratio of fan power consumption to vol flow rate\n",
+      "k = 200;    \t\t\t\t#[W/m.K] alumunium\n",
+      "Tsurr = 25+273.15;    \t\t#[K] Temperature of surrounding air\n",
+      "Tc = 56.4+273.15;    \t\t#[K] Temp of fuel cell\n",
+      "Rtcy = math.pow(10,-3);     #[K/W]   Contact thermal resistance\n",
+      "tb = .002;           \t\t#[m] thickness of base of heat sink\n",
+      "Lc = .05;        \t\t\t#[m] length of fuel cell\n",
+      "#Dimensions of Fin\n",
+      "tf = .001;    \t\t\t\t#[m] Thickness\n",
+      "Lf = .008;     \t\t\t\t#[m] Length\n",
+      "#calculations\n",
+      "\n",
+      "Vf = V*(Wc*(H-tc));    \t\t#[m^3/sec] Volumetric flow rate\n",
+      "Pnet = P - C*Vf;\n",
+      "\n",
+      "\n",
+      "P = 2*(Lc+tf);\n",
+      "Ac = Lc*tf;\n",
+      "N = 22;\n",
+      "a=(2*Wc - N*tf)/N;\n",
+      "h = 19.1;            \t\t#/[W/m^2.K]\n",
+      "q = 11.25;            \t\t#[W]\n",
+      "m = math.pow((h*P/(k*Ac)),.5);\n",
+      "Rtf = math.pow((h*P*k*Ac),(-.5))/ math.tanh(m*Lf);\n",
+      "Rtc = Rtcy/(2*Lc*Wc);\n",
+      "Rtbase = tb/(2*k*Lc*Wc);\n",
+      "Rtb = 1/(h*(2*Wc-N*tf)*Lc);\n",
+      "Rtfn = Rtf/N;\n",
+      "Requiv = 1/(1/Rtb + 1/Rtfn);\n",
+      "Rtot = Rtc + Rtbase + Requiv;\n",
+      "\n",
+      "Tc2 = Tsurr +q*(Rtot);\n",
+      "#results\n",
+      "\n",
+      "print '%s %.2f %s' %(\"\\n\\n (a) Power consumed by fan is more than the generated power of fuel cell, and hence system cannot produce net power = \",Pnet ,\"W \")\n",
+      "print '%s %.2f %s %.2f %s' %(\"\\n\\n (b) Actual fuel cell Temp is close enough to \",Tc2-273.,\" degC for reducing the fan power consumption by half ie Pnet =\",C*Vf/2.,\" W, we require 22 fins, 11 on top and 11 on bottom.\");\n",
+      "\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        " (a) Power consumed by fan is more than the generated power of fuel cell, and hence system cannot produce net power =  -0.40 W \n",
+        "\n",
+        "\n",
+        " (b) Actual fuel cell Temp is close enough to  54.47  degC for reducing the fan power consumption by half ie Pnet = 4.70  W, we require 22 fins, 11 on top and 11 on bottom.\n"
+       ]
+      }
+     ],
+     "prompt_number": 22
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example 3.12 Page 163"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "#Variable Initialization\n",
+      "\n",
+      "# Heat loss from body & temp at inner surface\n",
+      "import math\n",
+      "hair = 2.;     \t\t\t#[W/m^2.K] Heat convection coefficient air\n",
+      "hwater = 200.;     \t\t#[W/m^2.K] Heat convection coefficient water\n",
+      "hr = 5.9 ;     \t\t\t#[W/m^2.K] Heat radiation coefficient\n",
+      "Tsurr = 297.;    \t\t#[K] Temperature of surrounding air\n",
+      "Tc = 37+273.;    \t\t#[K] Temp inside\n",
+      "e = .95;\n",
+      "A = 1.8 ;       \t\t#[m^2] area\n",
+      "#Prop of blood\n",
+      "w = .0005 ;      \t\t#[s^-1] perfusion rate\n",
+      "pb = 1000.;        \t\t#[kg/m^3] blood density\n",
+      "cb = 3600.;        \t\t#[J/kg] specific heat\n",
+      "#Dimensions & properties of muscle & skin/fat\n",
+      "Lm = .03 ;       \t\t#[m]\n",
+      "Lsf = .003 ;     \t\t#[m]\n",
+      "km = .5 ;       \t\t#[W/m.K]\n",
+      "ksf = .3;        \t\t#[W/m.K]\n",
+      "q = 700.;         \t\t#[W/m^3]  Metabolic heat generation rate\n",
+      "#calculations\n",
+      "\n",
+      "Rtotair = (Lsf/ksf + 1/(hair + hr))/A;\n",
+      "Rtotwater = (Lsf/ksf + 1/(hwater+hr))/A;\n",
+      "#please correct this in the textbook. \n",
+      "m = math.pow((w*pb*cb/km),.5);\n",
+      "Theta = -q/(w*pb*cb);\n",
+      "\n",
+      "Tiair = (Tsurr*math.sinh(m*Lm) + km*A*m*Rtotair*(Theta + (Tc + q/(w*pb*cb))*math.cosh(m*Lm)))/(math.sinh(m*Lm)+km*A*m*Rtotair*math.cosh(m*Lm));\n",
+      "qair = (Tiair - Tsurr)/Rtotair;\n",
+      "\n",
+      "Tiwater = (Tsurr*math.sinh(m*Lm) + km*A*m*Rtotwater*(Theta + (Tc + q/(w*pb*cb))*math.cosh(m*Lm)))/(math.sinh(m*Lm)+km*A*m*Rtotwater*math.cosh(m*Lm));\n",
+      "qwater = (Tiwater - Tsurr)/Rtotwater;\n",
+      "#results\n",
+      "\n",
+      "print '%s %.2f %s' %(\"\\n\\n For Air \\n Temp excess Ti = \",Tiair-273,\" degC \")\n",
+      "print '%s %.2f %s %.2f %s %.2f %s' %(\"and Heat loss rate =\",qair,\" W \\n\\n For Water \\n Temp excess Ti = \",Tiwater-273,\" degC and Heat loss rate =\",qwater,\"W \");\n",
+      "#END"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "\n",
+        "\n",
+        " For Air \n",
+        " Temp excess Ti =  34.77  degC \n",
+        "and Heat loss rate = 141.99  W \n",
+        "\n",
+        " For Water \n",
+        " Temp excess Ti =  28.25  degC and Heat loss rate = 514.35 W \n"
+       ]
+      }
+     ],
+     "prompt_number": 23
+    }
+   ],
+   "metadata": {}
+  }
+ ]
+}
\ No newline at end of file