From c7fe425ef3c5e8804f2f5de3d8fffedf5e2f1131 Mon Sep 17 00:00:00 2001
From: hardythe1
Date: Tue, 7 Apr 2015 15:58:05 +0530
Subject: added books

---
 .../Chapter5_2.ipynb                               | 166 +++++++++++++++++++++
 1 file changed, 166 insertions(+)
 create mode 100755 Thermodynamics:_From_concepts_to_applications/Chapter5_2.ipynb

(limited to 'Thermodynamics:_From_concepts_to_applications/Chapter5_2.ipynb')

diff --git a/Thermodynamics:_From_concepts_to_applications/Chapter5_2.ipynb b/Thermodynamics:_From_concepts_to_applications/Chapter5_2.ipynb
new file mode 100755
index 00000000..7ebf1310
--- /dev/null
+++ b/Thermodynamics:_From_concepts_to_applications/Chapter5_2.ipynb
@@ -0,0 +1,166 @@
+{
+ "metadata": {
+  "name": "",
+  "signature": "sha256:4e735a3e117e4e268af257af7ccec75bd1ac3fad4a8f848db2d81766258e8e27"
+ },
+ "nbformat": 3,
+ "nbformat_minor": 0,
+ "worksheets": [
+  {
+   "cells": [
+    {
+     "cell_type": "heading",
+     "level": 1,
+     "metadata": {},
+     "source": [
+      "Chapter5 -The ideal gas"
+     ]
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example1-pg 66"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "import math\n",
+      "#calculate specific volumes at given pressure\n",
+      "##initialisation of variables\n",
+      "R= 8.314 ##J/mol K\n",
+      "M= 18.016 ##gms\n",
+      "T= 400. ##C\n",
+      "p= 0.01 ##Mpa\n",
+      "p1= 0.1 ##Mpa\n",
+      "p2= 20. ##Mpa\n",
+      "##CALCULATIONS\n",
+      "v= R*(273.156+T)/(M*p*1000)\n",
+      "v1= R*(273.156+T)/(M*p1*1000)\n",
+      "v2= R*(273.156+T)/(M*p2*1000)\n",
+      "##RESULTS\n",
+      "print'%s %.3f %s'%(' specific voulme =',v,'m^3/kg')\n",
+      "print'%s %.3f %s'%('specific voulme = ', v1,'m^3/kg')\n",
+      "print'%s %.3f %s'%('specific voulme = ',v2,'m^3/kg')\n"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        " specific voulme = 31.065 m^3/kg\n",
+        "specific voulme =  3.106 m^3/kg\n",
+        "specific voulme =  0.016 m^3/kg\n"
+       ]
+      }
+     ],
+     "prompt_number": 2
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "example 3-pg73 "
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "import math\n",
+      "#calculate final temperature and pressure and work ,energy\n",
+      "##initialisation of variables\n",
+      "p1= 300.##kPa\n",
+      "V1= 0.03 ##m^3\n",
+      "V2= 0.08 ##m^3\n",
+      "T1= 27. ##C\n",
+      "##CALCULATIONS1\n",
+      "T2= T1+273\n",
+      "p2= p1*(V1/V2)*(T2/(T1+273))\n",
+      "W= 0\n",
+      "Q= 0\n",
+      "##RESULTS\n",
+      "print'%s %.2f %s'%('final temperature =',T2,'K')\n",
+      "print'%s %.1f %s'%('final pressure =',p2,'kPa')\n",
+      "print'%s %.f %s'%('work = ',W,'kJ')\n",
+      "print'%s %.f %s'%('energy =',Q,'kJ')\n",
+      " \n"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        "final temperature = 300.00 K\n",
+        "final pressure = 112.5 kPa\n",
+        "work =  0 kJ\n",
+        "energy = 0 kJ\n"
+       ]
+      }
+     ],
+     "prompt_number": 9
+    },
+    {
+     "cell_type": "heading",
+     "level": 2,
+     "metadata": {},
+     "source": [
+      "Example4 -pg74\n",
+      "\n"
+     ]
+    },
+    {
+     "cell_type": "code",
+     "collapsed": false,
+     "input": [
+      "import math\n",
+      "#calculate mass of nitrogen and final temperature and piston rise\n",
+      "##initialisation of variables\n",
+      "p1= 2. ##Mpa\n",
+      "V1= 0.2 ##m^3\n",
+      "R= 8.314 ##J/mol K\n",
+      "T1= 500. ##C\n",
+      "M= 28. ##gms\n",
+      "p2= 0.3 ##Mpa\n",
+      "T2= 250 ##C\n",
+      "k= 1.4\n",
+      "A= 0.1 ##m^2\n",
+      "##CALCULATIONS\n",
+      "m1= p1*10*10*10*V1*M/(R*(273.15+T1))\n",
+      "m2= p2*10*10*10*V1*M/(R*(273.15+T2))\n",
+      "m3= -(m2-m1)\n",
+      "T3= (m1*(273.15+T1)-m2*(273.15+T2))/(k*m3)\n",
+      "z3= m3*R*T3/(p2*10*10*10*A*M)\n",
+      "##RESULTS\n",
+      "print'%s %.4f %s'%(' mass of nitrogen =',m3,'kg')\n",
+      "print'%s %.1f %s'%('final temperature =',T3,'K')\n",
+      "print'%s %.2f %s'%('piston rise =',z3,'m')\n"
+     ],
+     "language": "python",
+     "metadata": {},
+     "outputs": [
+      {
+       "output_type": "stream",
+       "stream": "stdout",
+       "text": [
+        " mass of nitrogen = 1.3561 kg\n",
+        "final temperature = 603.1 K\n",
+        "piston rise = 8.10 m\n"
+       ]
+      }
+     ],
+     "prompt_number": 11
+    }
+   ],
+   "metadata": {}
+  }
+ ]
+}
\ No newline at end of file
-- 
cgit