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, 183 insertions, 0 deletions

diff --git a/Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter3_7iK58pH.ipynb b/Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter3_7iK58pH.ipynb
new file mode 100644
index 00000000..e19c2f9d
--- /dev/null
+++ b/Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter3_7iK58pH.ipynb
@@ -0,0 +1,183 @@
+{

+ "metadata": {

+  "name": "",

+  "signature": "sha256:0241392dc5003b5a1bdb0f1da1ae62de4660e244f661b15b4862e3c841a68f3b"

+ },

+ "nbformat": 3,

+ "nbformat_minor": 0,

+ "worksheets": [

+  {

+   "cells": [

+    {

+     "cell_type": "heading",

+     "level": 1,

+     "metadata": {},

+     "source": [

+      "Chapter3-Two-dimensional Cascades"

+     ]

+    },

+    {

+     "cell_type": "heading",

+     "level": 2,

+     "metadata": {},

+     "source": [

+      "Ex1-pg77"

+     ]

+    },

+    {

+     "cell_type": "code",

+     "collapsed": false,

+     "input": [

+      "import math\n",

+      "#calculate the\n",

+      "a_l=0.5\n",

+      "alpha2=20.\n",

+      "theta=30.\n",

+      "##function to calculate m and delta\n",

+      "m = 0.23*(2*a_l)**2 + alpha2/500;\n",

+      "delta = m*theta;\n",

+      "\n",

+      "##given data\n",

+      "alpha1_ = 50;## in deg\n",

+      "alpha2_ = 20;## in deg\n",

+      "a_l = 0.5;##percentage\n",

+      "s_l = 1.0;\n",

+      "eps = 21;##in deg\n",

+      "\n",

+      "##Calculations\n",

+      "theta = alpha1_ - alpha2_;\n",

+      "alpha21 = 20;##in deg\n",

+      "alpha22 = 28.1;##in deg\n",

+      "\n",

+      "alpha23 = 28.6;##in deg\n",

+      "\n",

+      "alpha1 = eps + alpha23;\n",

+      "i = alpha1 - alpha1_;\n",

+      "alpham = (180./math.pi)*math.atan(0.5*(math.tan(alpha1*math.pi/180.) + math.tan(alpha23*math.pi/180.)));\n",

+      "CL = 2*(s_l)*math.cos(alpham*math.pi/180.)*(math.tan(alpha1*math.pi/180.) - math.tan(alpha23*math.pi/180.));\n",

+      "\n",

+      "##Results\n",

+      "print'%s %.2f %s'%('The fluid deflection = ',eps,' deg.');\n",

+      "print'%s %.2f %s'%('\\n The fluid deviation = ',i,' deg.');\n",

+      "print'%s %.2f %s'%('\\n The ideal lift coefficient at the design point = ',CL,'');\n"

+     ],

+     "language": "python",

+     "metadata": {},

+     "outputs": [

+      {

+       "output_type": "stream",

+       "stream": "stdout",

+       "text": [

+        "The fluid deflection =  21.00  deg.\n",

+        "\n",

+        " The fluid deviation =  -0.40  deg.\n",

+        "\n",

+        " The ideal lift coefficient at the design point =  0.95 \n"

+       ]

+      }

+     ],

+     "prompt_number": 1

+    },

+    {

+     "cell_type": "heading",

+     "level": 2,

+     "metadata": {},

+     "source": [

+      "Ex2-pg78"

+     ]

+    },

+    {

+     "cell_type": "code",

+     "collapsed": false,

+     "input": [

+      "import math\n",

+      "#calculate the\n",

+      "\n",

+      "##given data\n",

+      "s_l = 1.0;\n",

+      "alpha1_ = 50.;##in deg\n",

+      "alpha2_ = 20.;##in deg\n",

+      "eps_ = 21.;##in deg\n",

+      "i_ = -0.4;##in deg\n",

+      "i = 3.8;##in deg\n",

+      "CD = 0.017;\n",

+      "eps = 1.15*eps_;\n",

+      "\n",

+      "##Calculations\n",

+      "alpha1 = alpha1_+i;\n",

+      "alpha2 = alpha1-eps;\n",

+      "alpham = (180./math.pi)*math.atan(0.5*(math.tan(alpha1*math.pi/180.) + math.tan(alpha2*math.pi/180.)));\n",

+      "zeta = CD/((s_l)*(math.cos(alpham*math.pi/180.))**3);\n",

+      "Cf = 2.*(math.tan(alpha1*math.pi/180.) - math.tan(alpha2*math.pi/180.));\n",

+      "eff_D = 1 - zeta/(Cf*math.tan(alpham*math.pi/180.));\n",

+      "\n",

+      "##Results\n",

+      "print'%s %.2f %s'%('The tangential lift force coefficient = ',Cf,'');\n",

+      "print'%s %.2f %s'%('\\n The diffuser efficiency =  ',eff_D*100,'percentage.');\n"

+     ],

+     "language": "python",

+     "metadata": {},

+     "outputs": [

+      {

+       "output_type": "stream",

+       "stream": "stdout",

+       "text": [

+        "The tangential lift force coefficient =  1.59 \n",

+        "\n",

+        " The diffuser efficiency =   97.03 percentage.\n"

+       ]

+      }

+     ],

+     "prompt_number": 3

+    },

+    {

+     "cell_type": "heading",

+     "level": 2,

+     "metadata": {},

+     "source": [

+      "Ex3-pg83"

+     ]

+    },

+    {

+     "cell_type": "code",

+     "collapsed": false,

+     "input": [

+      "import math\n",

+      "import numpy\n",

+      "#calculate the\n",

+      "##given data\n",

+      "alpha1 = 58.;##in deg\n",

+      "alpha2 = 44.;##in deg\n",

+      "AVR = 1.0;\n",

+      "\n",

+      "##Calculations\n",

+      "alpham = (180./math.pi)*math.atan(0.5*(math.tan(alpha1*math.pi/180.) + math.tan(alpha2*math.pi/180.)));\n",

+      "zetam = (180./math.pi)*math.atan(math.tan(alpham*math.pi/180.) - 0.213);\n",

+      "Cpi = 1.-(math.cos(alpha1*math.pi/180.)/math.cos(alpha2*math.pi/180.))**2;\n",

+      "s_l = 9.*(0.567-Cpi);\n",

+      "theta = ((zetam-alpha2+1.1*(s_l)**(1/3.))/(0.5-0.31*(s_l)**(1/3.)));\n",

+      "delta = alpha2-zetam-0.5*theta;\n",

+      "print round(theta,2)\n",

+      "print round(s_l,2)\n",

+      "##Results\n",

+      "\n"

+     ],

+     "language": "python",

+     "metadata": {},

+     "outputs": [

+      {

+       "output_type": "stream",

+       "stream": "stdout",

+       "text": [

+        "21.08\n",

+        "0.99\n"

+       ]

+      }

+     ],

+     "prompt_number": 4

+    }

+   ],

+   "metadata": {}

+  }

+ ]

+}
\ No newline at end of file