{ "metadata": { "name": "", "signature": "sha256:b9f90dbe8cdd3ac15f14ed9a5dcea4d99b8c522db4806d23bf359fc881d94c73" }, "nbformat": 3, "nbformat_minor": 0, "worksheets": [ { "cells": [ { "cell_type": "heading", "level": 1, "metadata": {}, "source": [ "Chapter1-Fundamental concepts" ] }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Ex1-pg18" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math\n", "#calculate denisty of air and its mass\n", "p=2.*10**5; ## Pa\n", "T=300.; ## K\n", "R=287.; ## J/(kg.K)\n", "V=3.; ## m^3\n", "\n", "rho=p/(R*T);\n", "print'%s %.2f %s'%('The density of air =',rho,'kg/m^3')\n", "m=rho*V;\n", "print'%s %.2f %s'%('Its mass =',m,'m^3')\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "The density of air = 2.32 kg/m^3\n", "Its mass = 6.97 m^3\n" ] } ], "prompt_number": 1 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Ex2-pg19" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math\n", "#calculate gas constant Co ,Co2 ,No,N2o\n", "M_C=12.;\n", "M_N=14.;\n", "M_O=16.;\n", "R=8314.; ## J/(kg.K)\n", "\n", "M_CO=M_C+M_O;\n", "R_CO=R/M_CO;\n", "\n", "M_CO2=M_C+2.*M_O;\n", "R_CO2=R/M_CO2;\n", "\n", "M_NO=M_N+M_O;\n", "R_NO=R/M_NO;\n", "\n", "M_N2O=2.*M_N+M_O;\n", "R_N2O=R/M_N2O;\n", "\n", "print'%s %.1f %s'%('Gas constant for CO =',R_CO,'J/(kg.K)')\n", "print'%s %.1f %s'%('Gas constant for CO2 =',R_CO2,'J/(kg.K)')\n", "print'%s %.1f %s'%(\"Gas constant for NO =\",R_NO,\"J/(kg.K)\")\n", "print'%s %.1f %s'%(\"Gas constant for N2O =\",R_N2O,\"J/(kg.K)\")\n" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Gas constant for CO = 296.9 J/(kg.K)\n", "Gas constant for CO2 = 189.0 J/(kg.K)\n", "Gas constant for NO = 277.1 J/(kg.K)\n", "Gas constant for N2O = 189.0 J/(kg.K)\n" ] } ], "prompt_number": 3 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Ex3-pg36" ] }, { "cell_type": "code", "collapsed": false, "input": [ "import math\n", "#calculate reynodls number and prove the \n", "d=0.004; ## m\n", "rho=1000; ## kg/m^3\n", "v=3; ## m/s\n", "meu=10**(-3); ## khm(m.s)\n", "\n", "Re=rho*v*d/meu; \n", "print'%s %.f %s'%(\"Reynolds number =\",Re,\"\")\n", "\n", "print(\"The Reynolds number is well in excess of 4000, so the flow is turbulent.\")" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "Reynolds number = 12000 \n", "The Reynolds number is well in excess of 4000, so the flow is turbulent.\n" ] } ], "prompt_number": 4 } ], "metadata": {} } ] }