{ "cells": [ { "cell_type": "markdown", "metadata": {}, "source": [ "# Chapter 17 Gas cycles and processes" ] }, { "cell_type": "markdown", "metadata": {}, "source": [ "## Ex:17.1 Pg:768" ] }, { "cell_type": "code", "execution_count": 2, "metadata": { "collapsed": false }, "outputs": [ { "name": "stdout", "output_type": "stream", "text": [ "\n", " Thermal efficiency = 14.9 percent\n", "\n", " Moles of fuel burned per mol of air = 0.00177 mol fuel/mol air\n", "\n", " Mass ratio in pounds = 0.00866 lbm fuel/lbm air\n", "\n", " Air fuel ratio = 115 lbm air/lbm fuel\n" ] } ], "source": [ "from __future__ import division\n", "\n", "#Initialization of variables\n", "ha=1033 #Btu/mol air\n", "hbd=2992 #Btu/mol air\n", "hc=7823 #Btu/mol air\n", "hdd=5142 #Btu/mol air\n", "Hv=2733000 #Btu/mol\n", "M=29\n", "#calculations\n", "Wt=hc-hdd\n", "Wc=ha-hbd\n", "Net=Wt+Wc\n", "Heat=hc-hbd\n", "etat=Net*100/Heat\n", "molair=Heat/Hv\n", "mr=molair*142/M\n", "Af=1/mr\n", "#results\n", "print \"\\n Thermal efficiency = %.1f percent\"%(etat)\n", "print \"\\n Moles of fuel burned per mol of air = %.5f mol fuel/mol air\"%(molair)\n", "print \"\\n Mass ratio in pounds = %.5f lbm fuel/lbm air\"%(mr)\n", "print \"\\n Air fuel ratio = %d lbm air/lbm fuel\"%(Af)" ] } ], "metadata": { "kernelspec": { "display_name": "Python 2", "language": "python", "name": "python2" }, "language_info": { "codemirror_mode": { "name": "ipython", "version": 2 }, "file_extension": ".py", "mimetype": "text/x-python", "name": "python", "nbconvert_exporter": "python", "pygments_lexer": "ipython2", "version": "2.7.9" } }, "nbformat": 4, "nbformat_minor": 0 }