Added(A)/Deleted(D) following books

 A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_3ptASMI.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_4wHa84D.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_9JxFKFd.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_C7pfw6B.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_GqqK7m2.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_H0c7r3u.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_Iq2SYN6.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_KTU5lgY.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_O3VudAg.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_UKQHPIE.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_ZbMx9hO.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_dqq0jBY.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_mJo3HTQ.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_tWbQ8Pq.ipynb
A  A_Textbook_of_Electrical_Technology_AC_and_DC_Machines_by_A_K_Theraja_B_L_Thereja/chap_wCDB06c.ipynb
A  Advanced_Measurements_And_Instrumentation_by_A._K._Sawhney/Ch1_voXCiZP.ipynb
A  Advanced_Measurements_And_Instrumentation_by_A._K._Sawhney/Ch2_839zjBr.ipynb
A  Advanced_Measurements_And_Instrumentation_by_A._K._Sawhney/Ch3_JtKdjpi.ipynb
A  Advanced_Measurements_And_Instrumentation_by_A._K._Sawhney/Ch4_h6Jwto8.ipynb
A  Advanced_Measurements_And_Instrumentation_by_A._K._Sawhney/Ch5_2XUAsbf.ipynb
A  Advanced_Measurements_And_Instrumentation_by_A._K._Sawhney/Ch6_8Xtm119.ipynb
A  Advanced_Measurements_And_Instrumentation_by_A._K._Sawhney/screenshots/Screenshot_from_2_65JiggP.png
A  Advanced_Measurements_And_Instrumentation_by_A._K._Sawhney/screenshots/Screenshot_from_2_KYhBgvr.png
A  Advanced_Measurements_And_Instrumentation_by_A._K._Sawhney/screenshots/Screenshot_from_2_OJGeNYs.png
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/Chapter_10_Properties_Of__kgiORTS.ipynb
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/Chapter_11_Steam_Boilers_TQuXuTV.ipynb
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/Chapter_13_Steam_Engines_zTSDNSc.ipynb
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/Chapter_14_Air_Standard_C_m7SxTPj.ipynb
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/Chapter_2_Properties_Of_M_xMKkegG.ipynb
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/Chapter_5_Metrology_xHgz5kr.ipynb
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/Chapter_7_Fluid_Mechanics_VydgOYT.ipynb
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/Chapter_9__Laws_Of_Thermo_EMQgMuo.ipynb
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/screenshots/chapter10_iDXA5E5.png
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/screenshots/chapter14_zNTXzAs.png
A  Basic_mechanical_engineering_by_Basant_Agrawal_,_C.M_Agrawal/screenshots/chapter5_Ank30Hw.png
A  Electrical_and_Electronic_Systems_by_Neil_Storey/README.txt
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter10_4ctx213.ipynb
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter2_COfrarn.ipynb
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter3_7iK58pH.ipynb
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter4_YZTImEN.ipynb
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter5_T6xNkI8.ipynb
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter6_VZhkm5E.ipynb
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter7_2hkovpj.ipynb
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter8_Bt8FCnc.ipynb
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter9_TOCkwb3.ipynb
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/screenshots/Chapter10.png
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/screenshots/chapter6_Q3tBrTp.png
A  Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/screenshots/chapter7_qVshgvy.png
A  sample_notebooks/kumargugloth/Chapter1_wopEYRj.ipynb

1 files changed, 248 insertions, 0 deletions

diff --git a/Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter2_COfrarn.ipynb b/Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter2_COfrarn.ipynb
new file mode 100644
index 00000000..bb8ece3c
--- /dev/null
+++ b/Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter2_COfrarn.ipynb
@@ -0,0 +1,248 @@
+{

+ "metadata": {

+  "name": "",

+  "signature": "sha256:719cabf4d155b5060d8459b45f43cc016b1e1aad0e88a0a317b0beeb5ac9abba"

+ },

+ "nbformat": 3,

+ "nbformat_minor": 0,

+ "worksheets": [

+  {

+   "cells": [

+    {

+     "cell_type": "heading",

+     "level": 1,

+     "metadata": {},

+     "source": [

+      "Chapter2-Basic Thermodynamics, Fluid Mechanics: Definitions of Efficiency"

+     ]

+    },

+    {

+     "cell_type": "heading",

+     "level": 2,

+     "metadata": {},

+     "source": [

+      "Ex1-pg40"

+     ]

+    },

+    {

+     "cell_type": "code",

+     "collapsed": false,

+     "input": [

+      "import math\n",

+      "#calculate the polyefficency and overall total to total efficiency\n",

+      "\n",

+      "##given data\n",

+      "gamma = 1.4;\n",

+      "pi = 8.;##pressure ratio\n",

+      "T01 = 300.;##inlet temperature in K\n",

+      "T02 = 586.4;##outlet temperature in K\n",

+      "\n",

+      "##Calculations\n",

+      "##Calculation of Overall Total to Total efficiency\n",

+      "Tot_eff = ((pi**((gamma-1.)/gamma))-1.)/((T02/T01)-1.);\n",

+      "\n",

+      "##Calculation of polytropic efficiency\n",

+      "Poly_eff = ((gamma-1.)/gamma)*((math.log(pi))/math.log(T02/T01));\n",

+      "\n",

+      "##Results\n",

+      "print'%s %.2f %s'%('The Overall total-to-total efficiency is ',Tot_eff,'');\n",

+      "print'%s %.2f %s'%('The polytropic efficiency is ',Poly_eff,'');\n"

+     ],

+     "language": "python",

+     "metadata": {},

+     "outputs": [

+      {

+       "output_type": "stream",

+       "stream": "stdout",

+       "text": [

+        "The Overall total-to-total efficiency is  0.85 \n",

+        "The polytropic efficiency is  0.89 \n"

+       ]

+      }

+     ],

+     "prompt_number": 1

+    },

+    {

+     "cell_type": "heading",

+     "level": 2,

+     "metadata": {},

+     "source": [

+      "Ex2-pg44"

+     ]

+    },

+    {

+     "cell_type": "code",

+     "collapsed": false,

+     "input": [

+      "import math\n",

+      "#calculate the\n",

+      "\n",

+      "##given data\n",

+      "T01 = 1200.;##Stagnation temperature at which gas enters in K\n",

+      "p01 = 4.;##Stagnation pressure at which gas enters in bar\n",

+      "c2 = 572.;##exit velocity in m/s\n",

+      "p2 = 2.36;##exit pressure in bar\n",

+      "Cp = 1.160*1000.;##in J/kgK\n",

+      "gamma = 1.33\n",

+      "\n",

+      "##calculations\n",

+      "T2 = T01 - 0.5*(c2**2)/Cp;##Calculation of exit temperature in K\n",

+      "Noz_eff = ((1.-(T2/T01))/(1.-(p2/p01)**((gamma-1.)/gamma)));##Nozzle efficiency\n",

+      "\n",

+      "##Results\n",

+      "print'%s %.2f %s'%('Nozzle efficiency is ',Noz_eff,'');\n"

+     ],

+     "language": "python",

+     "metadata": {},

+     "outputs": [

+      {

+       "output_type": "stream",

+       "stream": "stdout",

+       "text": [

+        "Nozzle efficiency is  0.96 \n"

+       ]

+      }

+     ],

+     "prompt_number": 2

+    },

+    {

+     "cell_type": "heading",

+     "level": 2,

+     "metadata": {},

+     "source": [

+      "Ex3-pg51"

+     ]

+    },

+    {

+     "cell_type": "code",

+     "collapsed": false,

+     "input": [

+      "import math\n",

+      "#calculate the\n",

+      "\n",

+      "##given data\n",

+      "cp = 0.6;##coefficient of pressure\n",

+      "AR = 2.13;##Area ratio\n",

+      "N_R1 = 4.66;\n",

+      "\n",

+      "##calculations\n",

+      "cpi = 1. - (1./(AR**2));\n",

+      "Diff_eff = cp/cpi;##diffuser efficiency\n",

+      "theta = 2.*(180./math.pi)*math.atan((AR**0.5 - 1.)/(N_R1));##included cone angle\n",

+      "\n",

+      "##Results\n",

+      "print'%s %.2f %s'%('cpi = \\n',cpi,'');\n",

+      "print'%s %.2f %s'%('The included cone angle can be found = ',theta,' deg.');\n",

+      "\n",

+      "\n"

+     ],

+     "language": "python",

+     "metadata": {},

+     "outputs": [

+      {

+       "output_type": "stream",

+       "stream": "stdout",

+       "text": [

+        "cpi = \n",

+        " 0.78 \n",

+        "The included cone angle can be found =  11.26  deg.\n"

+       ]

+      }

+     ],

+     "prompt_number": 4

+    },

+    {

+     "cell_type": "heading",

+     "level": 2,

+     "metadata": {},

+     "source": [

+      "Ex4-pg52"

+     ]

+    },

+    {

+     "cell_type": "code",

+     "collapsed": false,

+     "input": [

+      "import math\n",

+      "#calculate the\n",

+      "\n",

+      "##given data\n",

+      "AR = 1.8;##Area ratio\n",

+      "cp = 0.6;##coefficient of pressure\n",

+      "N_R1 = 7.85;\n",

+      "\n",

+      "##calculations\n",

+      "Theta = 2.*(180./math.pi)*math.atan((AR**0.5 - 1.)/(N_R1));##included cone angle\n",

+      "cpi = 1.-(1./(AR**2));\n",

+      "Diff_eff = cp/cpi;##diffuser efficeincy\n",

+      "\n",

+      "##Results\n",

+      "print'%s %.2f %s'%('The included cone angle can be found = ',Theta,' deg.\\n');\n",

+      "print'%s %.2f %s'%('cpi = \\n',cpi,'');\n",

+      "print'%s %.2f %s'%('Diffuser efficiency = ',Diff_eff,'');\n"

+     ],

+     "language": "python",

+     "metadata": {},

+     "outputs": [

+      {

+       "output_type": "stream",

+       "stream": "stdout",

+       "text": [

+        "The included cone angle can be found =  4.98  deg.\n",

+        "\n",

+        "cpi = \n",

+        " 0.69 \n",

+        "Diffuser efficiency =  0.87 \n"

+       ]

+      }

+     ],

+     "prompt_number": 5

+    },

+    {

+     "cell_type": "heading",

+     "level": 2,

+     "metadata": {},

+     "source": [

+      "Ex5-pg53"

+     ]

+    },

+    {

+     "cell_type": "code",

+     "collapsed": false,

+     "input": [

+      "import math\n",

+      "#calculate the\n",

+      "\n",

+      "##given data\n",

+      "AR = 2.0;##Area ratio\n",

+      "alpha1 = 1.059;\n",

+      "B1 = 0.109;\n",

+      "alpha2 = 1.543;\n",

+      "B2 = 0.364;\n",

+      "cp = 0.577;##coefficient of pressure\n",

+      "\n",

+      "##calculations\n",

+      "cp = (alpha1 - (alpha2/(AR**2))) - 0.09;\n",

+      "Diff_eff = cp/(1.-(1./(AR**2)));##Diffuser efficiency\n",

+      "\n",

+      "##Results\n",

+      "print'%s %.2f %s'%('The diffuser efficiency = ',Diff_eff,'');\n"

+     ],

+     "language": "python",

+     "metadata": {},

+     "outputs": [

+      {

+       "output_type": "stream",

+       "stream": "stdout",

+       "text": [

+        "The diffuser efficiency =  0.78 \n"

+       ]

+      }

+     ],

+     "prompt_number": 6

+    }

+   ],

+   "metadata": {}

+  }

+ ]

+}
\ No newline at end of file