From 400c5d4d1987e66daeb868c8de422d666f959e7f Mon Sep 17 00:00:00 2001 From: Trupti Kini Date: Tue, 3 Jan 2017 23:30:39 +0600 Subject: 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 --- .../Chapter2_COfrarn.ipynb | 248 +++++++++++++++++++++ 1 file changed, 248 insertions(+) create mode 100644 Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter2_COfrarn.ipynb (limited to 'Fluid_Mechanics,Thermodynamics_of_Turbomachinery_by_S.L.Dixon/Chapter2_COfrarn.ipynb') 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 -- cgit