{ "metadata": { "name": "", "signature": "sha256:3a5f70d3bf4cb3a553b5fa0666639707f168933e92d2f8256330898382eb0c39" }, "nbformat": 3, "nbformat_minor": 0, "worksheets": [ { "cells": [ { "cell_type": "heading", "level": 1, "metadata": {}, "source": [ "CHAPTER 7: COMBUSTION BOILER TRIALS" ] }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.1 Page112" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "C=86#percent\n", "h=4.2#percent\n", "w=20#lb\n", "a=w+0.902#lb\n", "C2=44/12#lb\n", "N=0.77#lb\n", "CO2=3.15\n", "H2O=0.042*9#lb\n", "N2=w*N#lb\n", "Ox=a-CO2-H2O-N2#lb\n", "\n", "#CALCULATIONS\n", "Co2=CO2/a*100#percent\n", "H2o=H2O/a*100#percent\n", "n2=N2/a#percent\n", "o2=Ox/a*100#percent\n", "\n", "#RESULTS\n", "print\"The composition of the products of combutions by weight is\",round(o2,3),\"%\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "The composition of the products of combutions by weight is 9.444 %\n" ] } ], "prompt_number": 1 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.2 Page 113" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "g=0.05#percent\n", "n=0.35#percent\n", "c=0.5#percent\n", "h=10#percent\n", "m=167#C H U\n", "h1=162#C H U\n", "v=1#ft^3\n", "H2=0.5#ft^3\n", "Co=0.05#ft^3\n", "v2=3#ft\n", "\n", "#CALCULATIONS\n", "G=(g*c)+(n*H2)#ft^3\n", "Tv=(g*h1)+(n*m)#C H U\n", "M=Tv/v2#C H U/ft^3\n", "\n", "#RESULTS\n", "print\"The gas with twice its volume of air is\",round(M,3),\"C.H.U/ft^3\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "The gas with twice its volume of air is 22.183 C.H.U/ft^3\n" ] } ], "prompt_number": 2 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.4 Page 114" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "g=8#percent\n", "f=88#percent\n", "C=12#percent\n", "w=20#lb\n", "C1=11/3#lb\n", "CO2=3/11#lb\n", "e=0.08#lb\n", "D=0.0218#lb C\n", "w1=0.88#lb\n", "\n", "#CALCULATIONS\n", "W1=w1/D#lb lb fuel\n", "T=w1/D*w#lb/hr\n", "\n", "#RESULTS\n", "print\"the total weight of exaust gas leaving the engine per hour is\",round(T,3),\"lb/hr\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "the total weight of exaust gas leaving the engine per hour is 807.339 lb/hr\n" ] } ], "prompt_number": 4 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.6 Page 116" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "a=30#percent\n", "b=20#percent\n", "c=8#percent\n", "h=42#percent\n", "t1=20#degree C\n", "g=0.24#in\n", "t2=320#degree c\n", "M=7.654#lb/lb fuel\n", "A=3*M#lb/lb fuel\n", "W=0.08+0.04#lb\n", "T=A+0.8#lb\n", "w1=0.72+0.3#lb\n", "w=T-w1#lb\n", "d=w*0.24*(t2-b)#C H U/lb fuel\n", "H=1.02*(639+0.49*220-t1)#C H U/lb fuel\n", "\n", "#CALCULATIONS\n", "T1=d+H#C H U/lb fuel\n", "\n", "#RESULTS\n", "print\"total heat carried away by flue gases is\",round(T1,3),\"C H U/lb fuel\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "total heat carried away by flue gases is 2378.76 C H U/lb fuel\n" ] } ], "prompt_number": 5 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.7 Page 117" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "h=40#percent\n", "g=30#percent\n", "c=8#percent\n", "n=10#percent\n", "w=6#percent\n", "g1=10#percent\n", "g2=4.14#ft^3\n", "Ch4=4.562#ft^3 of air\n", "Co2=0.44#ft\n", "H2o=1.18#ft^3\n", "N2=3.7#ft63\n", "x=41.4/11#ft63\n", "\n", "#CALCULATIONS\n", "T=Ch4+x#ft^3\n", "v=1+T#ft^3\n", "V=x+g2#ft^3\n", "D=v-V#ft^3\n", "P=D/v*100#percent\n", "\n", "#RESULTS\n", "print\"the volueme of air suplied per is\",round(P,3),\"%\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "the volueme of air suplied per is 15.248 %\n" ] } ], "prompt_number": 6 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.9 Page 119" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "Ox=2.679#lb\n", "O2=Ox-0.03#lb O2/lb fuel\n", "o2=O2*100.0/23.0#lb air lb fuel\n", "E=o2/2.0#lb\n", "a=17.325#lb /lb fuel\n", "Co2=3.294#lb\n", "H2o=0.315#lb\n", "N2o=13.34#lb\n", "O2=23.0/100.0*E#lb\n", "So2=0.005*2#lb\n", "\n", "#CALCULATIONS\n", "W=Co2+N2o+O2+So2#lb /lb fuel\n", "\n", "#RESULTS\n", "print\"the total weight of dry products is\",round(W,3),\"lb /lb fuel\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "the total weight of dry products is 17.969 lb /lb fuel\n" ] } ], "prompt_number": 9 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.11 Page 120" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "l=8.7#percent\n", "Co2=42.0#percent\n", "N=28.0#percent\n", "O2=32.0#percent\n", "x=27.65#lb air\n", "W=(O2/12.0)*(100.0/23.0)#lb\n", "\n", "#CALCULATIONS\n", "A=x-W#lb\n", "\n", "#RESULTS\n", "print\"the air to flues /lb carbon is\",round(A,3),\"lb\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "the air to flues /lb carbon is 16.056 lb\n" ] } ], "prompt_number": 11 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.13 Page 121" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "Co=2420#C H U\n", "a=3400/6#C H U\n", "R=Co/3246#C H U\n", "T=1+0.745#lb\n", "n=1.12 #lb\n", "O2=1.33/1.745#lb\n", "C=O2*100/23#lb\n", "CB=n/T#lb\n", "m=1.74#lb\n", "k=2.33#lb\n", "l=1.33#lb\n", "c=77#lb\n", "d=23#lb\n", "\n", "#CALCULATIONS\n", "Y=l*c/d#N2\n", "\n", "#RESULTS\n", "print\"the weight of air and steam is\",round(Y,3),\"N2\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "the weight of air and steam is 4.453 N2\n" ] } ], "prompt_number": 12 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.15 Page 123" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "w=20#lb\n", "t=320#degree C\n", "t1=22#Degree C\n", "w1=0.0807#lb\n", "A=0.03901#AH\n", "W=0.07469#AH\n", "g=5.2#A\n", "Q=W-A#A\n", "\n", "#CALCULATIONS\n", "H=(g*0.625)/(Q)#ft\n", "\n", "#RESULTS\n", "print\"weight of equal column of external air is\",round(H,3),\"ft\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "weight of equal column of external air is 91.087 ft\n" ] } ], "prompt_number": 13 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.16 Page 124" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "p=120#lb/in^2\n", "h=30#in\n", "t=48#degree C\n", "C=1000#lb\n", "t1=26#degree C\n", "m=2.2#percent\n", "g=18#lb\n", "f=127#lb\n", "j=33000#in\n", "q=1400#in\n", "L=0.978*8000#C.H.U\n", "b=50#in\n", "t2=320#degree C\n", "g1=0.24#in\n", "d=0.90#in\n", "a=0.4912*30#lb/in^2\n", "P=p+a#lb/in^2 abs\n", "T=178.62+d*483.45#C.H.U/lb\n", "\n", "#CALCULATIONS\n", "Wt=C/f#lb\n", "H=Wt*(T-t)#C.H.U\n", "F=0.022*(638.9+0.48*220-t1)#C.H.U\n", "G=g*0.24*(t2-t1)#C.H.U\n", "E=H/L*100#percent\n", "E1=b*j*60/(L*f*q)*100#percent\n", "\n", "#RESULTS\n", "print\"the heat balance for the boiler and find its efficiency and the overall efficiency of the plant is\",round(E1,3),\"%\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "the heat balance for the boiler and find its efficiency and the overall efficiency of the plant is 7.117 %\n" ] } ], "prompt_number": 14 }, { "cell_type": "heading", "level": 2, "metadata": {}, "source": [ "Example 7.17 Page 126" ] }, { "cell_type": "code", "collapsed": false, "input": [ "#initialisation of variable\n", "from math import pi,sqrt,acos,asin,atan,cos,sin,tan\n", "v=7950#lb C.H.U /lb\n", "w=15#percent\n", "c=0.85#lb\n", "w1=14#percent\n", "w2=9#percent\n", "t1=15#degree C\n", "t2=325#degree C\n", "g=0.25#lb\n", "\n", "#CALCULATIONS\n", "H=c*v#C.H.U\n", "H1=0.15*(638.9+0.48*225-15)#C.H.U\n", "C=c*c#lb\n", "A=19.2#lb\n", "Wt=A+C#lb\n", "P=Wt*g*(t2-t1)#C.H.U/lb coal\n", "R=0.14*H#C.H.U\n", "R1=H-H1-P-R#C.H.U\n", "B=R1/H*100#percent\n", "\n", "#RESULTS\n", "print\"the efficiency of a boiler is\",round(B,3),\"%\"" ], "language": "python", "metadata": {}, "outputs": [ { "output_type": "stream", "stream": "stdout", "text": [ "the efficiency of a boiler is 61.527 %\n" ] } ], "prompt_number": 15 } ], "metadata": {} } ] }