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author | priyanka | 2015-06-24 15:03:17 +0530 |
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committer | priyanka | 2015-06-24 15:03:17 +0530 |
commit | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (patch) | |
tree | ab291cffc65280e58ac82470ba63fbcca7805165 /1943/CH4 | |
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Diffstat (limited to '1943/CH4')
-rwxr-xr-x | 1943/CH4/EX4.1/Ex4_1.sce | 39 | ||||
-rwxr-xr-x | 1943/CH4/EX4.10/Ex4_10.sce | 20 | ||||
-rwxr-xr-x | 1943/CH4/EX4.11/Ex4_11.sce | 39 | ||||
-rwxr-xr-x | 1943/CH4/EX4.12/Ex4_12.sce | 24 | ||||
-rwxr-xr-x | 1943/CH4/EX4.13/Ex4_13.sce | 47 | ||||
-rwxr-xr-x | 1943/CH4/EX4.2/Ex4_2.sce | 18 | ||||
-rwxr-xr-x | 1943/CH4/EX4.3/Ex4_3.sce | 23 | ||||
-rwxr-xr-x | 1943/CH4/EX4.4/Ex4_4.sce | 51 | ||||
-rwxr-xr-x | 1943/CH4/EX4.5/Ex4_5.sce | 34 | ||||
-rwxr-xr-x | 1943/CH4/EX4.6/Ex4_6.sce | 33 | ||||
-rwxr-xr-x | 1943/CH4/EX4.7/Ex4_7.sce | 19 | ||||
-rwxr-xr-x | 1943/CH4/EX4.8/Ex4_8.sce | 31 | ||||
-rwxr-xr-x | 1943/CH4/EX4.9/Ex4_9.sce | 27 |
13 files changed, 405 insertions, 0 deletions
diff --git a/1943/CH4/EX4.1/Ex4_1.sce b/1943/CH4/EX4.1/Ex4_1.sce new file mode 100755 index 000000000..7c59f44cd --- /dev/null +++ b/1943/CH4/EX4.1/Ex4_1.sce @@ -0,0 +1,39 @@ + +clc
+clear
+//Input data
+C=84;//The mass of carbon present in the fuel in %
+H=10;//The mass of hydrogen present in the fuel in %
+S=3.2;//The mass of sulphur present in the fuel in %
+O=1.6;//The mass of oxygen present in the fuel in %
+I=1.2;//The mass of incombustible in the fuel in %
+X=15.72;//The flue gas of combined CO2 and SO2 by volume in %
+Og=1;//The flue gas of O2 by volume in %
+Y=100;//Let us consider the fuel oil in kg
+C1=12;//Molecular weight of Carbon
+H1=2;//Molecular weight of hydrogen
+S1=32;//Molecular weight of sulphur
+O1=32;//Molecular weight of oxygen
+Co2=44;//Molecular weight of carbondioxide
+So2=64;//Molecular weight of sulphurdioxide
+N1=28;//Molecular weight of nitrogen
+H2O=18;//Molecular weight of water
+
+//Calculations
+b=C/C1;//Equating coefficients of the carbon from equation
+g=H/H1;//Equating coefficients of the hydrogen from equation
+d=S/S1;//Equating coefficients of the sulphur from the equation
+e=(b+d)/(X/Og);//By volumetric analysis
+x=b+d+e+(g/2)-(O/O1);//Moles of oxygen are supplied for combustion
+f=3.76*x;//Equating coefficients of the nitrogen from equation
+Mo=x*O1;//Mass of oxygen supplied in kg
+Ma=Mo/0.232;//Mass of air supplied for 100 kg of fuel in kg
+Wa=Ma/100;//Mass of air supplied for 1 kg fuel in kg
+Wrh={(11.5*C)+(34.5*[(H)-(O/8)])+(4.3*S)}/100;//Theoretical air required per kg of fuel in kg
+E=[(Wa-Wrh)/Wrh]*100;//Percentage of excess air in %
+D=(b*Co2)+(d*So2)+(e*O1)+(f*N1);//Mass of dry flue gas formed for 100 kg fuel in kg
+dfg=D/100;//Mass of dry flue gas formed per kg of fuel in kg
+Mw=(g*H2O)/100;//Mass of water vapour formed per kg of fuel
+
+//Output
+printf('(a) Mass of air supplied WA = %3.2f kg \n (b)Percentage excess air supplied = %3.2f percentage \n (c)mass of dry flue gas formed = %3.2f kg \n (d) Mass of water vapour formed = %3.2f kg',Wa,E,dfg,Mw)
diff --git a/1943/CH4/EX4.10/Ex4_10.sce b/1943/CH4/EX4.10/Ex4_10.sce new file mode 100755 index 000000000..62f265176 --- /dev/null +++ b/1943/CH4/EX4.10/Ex4_10.sce @@ -0,0 +1,20 @@ + +clc
+clear
+//Input data
+tg=180;//The gas temperature in degree centigrade
+p=250;//The draught produced by the ID fan in mm
+nf=0.52;//The efficiency of the fan
+Va=0.858;//Volume flow rate of air in m^3/kg
+g=9.812;//gravitational force constant in m/s^2
+Wf=10;//Coal rate in t/h
+Wa=12.9;//Actual air required per kg fuel in kg air/kg fuel
+ta=30;//Room temperature in degree centigrade
+
+//Calculations
+Wfg=[(Wf+(Wa*10))*1000]/3600;//Fuel gas required in kg/s
+Vfg=[Va*(tg+273)]/(ta+273);//Volume flow rate of fuel gas in m^3/kg
+ID=((Wfg*Vfg*p*g)/(nf))/1000;//ID fan motor capacity in kW
+
+//Output
+printf('The motor capacity of the ID fan is %3.2f kW ',ID)
diff --git a/1943/CH4/EX4.11/Ex4_11.sce b/1943/CH4/EX4.11/Ex4_11.sce new file mode 100755 index 000000000..0004d7fb9 --- /dev/null +++ b/1943/CH4/EX4.11/Ex4_11.sce @@ -0,0 +1,39 @@ + +clc
+clear
+//Input data
+CO2=13.2;//The volume of carbondioxide present in the partial analysis of dry flue gas in %
+O2=3.2;//The volume of oxygen present in the partial analysis of dry flue gas in %
+C=88;//The mass of carbon present in the coal according to coal analysis on mass basis in %
+H=4.4;//The mass of hydrogen present in the coal according to coal analysis on mass basis in %
+A=7.6;//The mass of ash present in the coal according to coal analysis on mass basis in %
+M=0;//Moisture present in the fuel was nil
+Mc=12;//Molecular weight of the carbon
+Mh=2;//Molecular weight of the hydrogen
+Mo=32;//Molecular weight of the oxygen
+Mho=18;//Molecular weight of water
+p=101.325;//Atmospheric pressure in kPa
+
+//Calculations
+c=C/Mc;//Equating coefficients of the carbon from the equation
+g=H/Mh;//Equating coefficients of the hydrogen from the equation
+x=(CO2/100)/(O2/100);//From dry fuel gas analysis (dfg)
+d=[[(CO2/100)*(47.5)]-7.333]/[[(CO2/100)*(3.032)]-1];//Coefficient of the carbonmonoxide in the equations product side
+b=c-d;//Coefficient of the carbondioxide in the equation product side
+a=10.21-(0.742*d);//Coefficient of the oxygen in the reactant side of the equation
+e=b/x;//Coefficient of the oxygen in the product side of the equation
+f=3.76*a;//Equating coefficients of the nitrogen from the equation
+ma=(a*Mo)/0.232;//Mass of air supplied for 100 kg coal in kg
+ma1=ma/100;//Mass of air supplied per kg coal in kg
+T=b+d+e+f;//Total number of moles of dry flue gas (dfg)
+CO21=(b/T)*100;//Carbondioxide by volume in percentage
+O21=(e/T)*100;//Oxygen by volume in percentage
+CO1=(d/T)*100;//Carbonmonoxide by volume in percentage
+N21=(f/T)*100;//Nitrogen by volume in percentage
+Mwv=(g*Mho)/100;//Mass of watervapour formed per kg coal in kg
+Mf=(g)/(b+d+e+f+g);//Mole fraction of water vapour in flue gas
+P=Mf*p;//Partial pressure of water vapour in kPa
+D=32.9;//Dew point temperature from steam tables in degree centigrade
+
+//Output
+printf('(a)The complete volumetric composition of the dry flue gas is \n Carbondioxide by volume = %3.2f percentage \n Oxygen by volume = %3.2f percentage \n Carbonmonoxide by volume = %3.2f percentage \n Nitrogen by volume = %3.2f percentage \n (b) The actual amount of air supplied per kg coal = %3.2f kg \n (c) Mass of water vapour formed per kg coal = %3.2f kg \n (d) The dew point temperature of the flue gas = %3.2f degree centigrade ',CO21,O21,CO1,N21,ma1,Mwv,D)
diff --git a/1943/CH4/EX4.12/Ex4_12.sce b/1943/CH4/EX4.12/Ex4_12.sce new file mode 100755 index 000000000..87adcf53a --- /dev/null +++ b/1943/CH4/EX4.12/Ex4_12.sce @@ -0,0 +1,24 @@ + +clc
+clear
+//Input data
+H=200;//Height of the stack in m
+D=4;//Diameter of the stack in m
+m=1000;//Mass flow rate of gas in kg/s
+Ts=100;//Stack exit gas temperature in degree centigrade
+Ta=5;//Ambient air temperature in degree centigrade
+Vw=50;//Wind velocity in Km/h
+Cp=1.005;//Specific heat of the gas in kJ/kgK
+pi=3.142;//Mathematical constant the value of pi
+
+//Calculations
+Vw1=(50*1000)/(60*60);//Wind velocity in m/s
+Qe=m*Cp*(Ts-Ta);//Heat emission from plume in kW
+Qe1=Qe/1000;//Heat emission from the plume in MW
+p=(101.325)/(0.287*373);//Density of the gas in kg/m^3
+A=(pi*D^2)/4;//Area of the stack in m^2
+Vs=m/(p*A);//Stack gas exict velocity in m/s
+H1=[(2.62*(Qe1^(1/2))*1000)/Vw1]-[(0.029*Vs*D)/Vw1];//The height of the gas plume in m
+
+//Output
+printf('The height of the gas plume is H = %3.1f m ',H1)
diff --git a/1943/CH4/EX4.13/Ex4_13.sce b/1943/CH4/EX4.13/Ex4_13.sce new file mode 100755 index 000000000..b6bd4e83b --- /dev/null +++ b/1943/CH4/EX4.13/Ex4_13.sce @@ -0,0 +1,47 @@ + +clc
+clear
+//Input data
+CV=20;//Calorific value of the fuel in MJ/kg
+C=65;//The amount of carbon present in the fuel according to gravimetric analysis in %
+H=25;//The amount of hydrogen present in the fuel according to gravimetric analysis in %
+O=10;//The amount of oxygen present in the fuel according to gravimetric analysis in %
+p1=1;//Pressure at the inlet of the compressor in bar
+t1=27;//Temperature at the inlet of the compressor in degree centigrade
+p2=4;//The pressure which compressor compresses it isentropically in bar
+Re=78;//The regenerator effectiveness in %
+CO2=6;//The amount of carbondioxide according to the analysis of dry exhaust gas in %
+CO=1.5;//The amount of carbonmonoxide according to the analysis of dry exhaust gas in %
+Cp=1.005;//Specific heat capacity of the air in kJ/kgK
+i=1.44;//Isentropic index for the air
+Cp1=1.15;//Specific heat capacity of the air in kJ/kgK
+i1=1.33;//Isentropic index for the combustion products
+Mc=12;//Molecular weight of the carbon
+Mh=2;//Molecular weight of the hydrogen
+Mo=32;//Molecular weight of the oxygen
+Mho=18;//Molecular weight of water
+T0=288;//Datum temperature in K (Assumed)
+
+//Calculations
+h=(C/100)/(Mc);//Equating coefficients of the carbon from the equation
+e=(H/100)/Mh;//Equating coefficients of the hydrogen from the equation
+y=(CO/100)/(CO2/100);//From dry exhaust gas analysis for solving
+a=h/(1+y);//The coefficient of the carbondioxide in the product side of the equation
+b=h-a;//The coefficient of the carbonmonoxide in the product side of the equation
+z=b/(CO/100);//The sum of coefficients of the product side of the equation
+x=z-(b/2)+(e/2);//Mol of air supplied in kmol
+wa=x*28.96;//Air supplied in kg/kg fuel
+wf=1;//Assuming 1 kg of fuel supplied
+T2=(t1+273)*(p2/p1)^((i-1)/i);//Temperature at the outlet of the compressor in K
+T3=[[(wa*Cp*(T2-T0))+(wf*CV*1000)]/[(wa+wf)*(Cp1)]]+T0;//Maximum temperature of the cycle in K
+T4=T3/[(4)^((i1-1)/i1)];//Temperature at point of the cycle in K
+T5=[(Re/100)*(T4-T2)]+T2;//Temperature at point of the cycle in K
+Wc=wa*Cp*(T2-(t1+273));//Work done by the compressor in kW
+Wt=23.54*Cp1*(T3-T4);//Work done by the turbine in kW
+Q1=23.54*Cp1*(T3-T5);//Total work done by the system in kW
+nc=(Wt-Wc)/Q1;//Efficiency of the cycle
+nc1=nc*100;//Efficiency of the cycle in %
+spc=3600/(Wt-Wc);//Specific fuel consumption in kg/kWh
+
+//Output
+printf('(a) The maximum temperature of the cycle T3 = %3.0f K \n (b)Thermal efficiency of the plant = %3.3f or %3.2f percentage\n (c) Specific fuel consumption = %3.3f kg/kWh ',T3,nc,nc1,spc)
diff --git a/1943/CH4/EX4.2/Ex4_2.sce b/1943/CH4/EX4.2/Ex4_2.sce new file mode 100755 index 000000000..d54483c56 --- /dev/null +++ b/1943/CH4/EX4.2/Ex4_2.sce @@ -0,0 +1,18 @@ + +clc
+clear
+//Input data
+CO2=11.5;//Percentage of carbondioxide present in combustion in %
+O2=2.7;//Percentage of oxygen present in the combustion in %
+CO=0.7;//Percentage of carbonmonoxide present in the combuston in %
+
+//Calculations
+a=85.1/3.76;//Equating moles for nitrogen from the equation
+x=(CO2+CO)/3;//Equating moles for carbon from the equation
+b=[a-CO2-(CO/2)-O2]*2;//Equating moles for oxygen from the equation
+y=a/x;//Moles of oxygen supplied for one mole of propane gas
+z=5;//Theoretically 5 moles of oxygen are required for reacting
+E=[(y-z)/z]*100;//The excess of air supplied in %
+
+//Output
+printf('The percentage excess air used is = %3.1f percentage',E)
diff --git a/1943/CH4/EX4.3/Ex4_3.sce b/1943/CH4/EX4.3/Ex4_3.sce new file mode 100755 index 000000000..aba54e17b --- /dev/null +++ b/1943/CH4/EX4.3/Ex4_3.sce @@ -0,0 +1,23 @@ + +clc
+clear
+//Input data
+CO2=12.1;//The amount of carbondioxide released from the combustion in %
+O2=3.8;//The amount of oxygen released from the combustion in %
+CO=0.9;//The amount of carbonmonoxide released from the combustion in %
+MO=32;//Molecular weight of Oxygen
+
+//Calculations
+a=83.2/3.76;//Equating moles for nitrogen from the equation
+b=(2*a)-(2*CO2)-(2*O2)-CO;//Equating moles for oxygen from the equation
+x=CO2+CO;//Equating moles for carbon from the equation
+y=2*b;//Equating moles for hydrogen from the equation
+z=18.75;//Moles of Oxygen from the stoichiometric equation
+z1=a;//Moles of Oxygen from the combustion equation
+E=[(z1-z)/z]*100;//Percentage of excess air in%
+A=(a*MO)/0.232;//Actual air supplied per mole of C13H23
+Mc=179;//Molecular weight of C13H23
+Af=A/Mc;//Air fuel ratio during the test
+
+//Output
+printf('(a) The air fuel ratio during the test = %3.2f \n (b) The excess or deficiency of air used = %3.0f Percentage of excess air used',Af,E)
diff --git a/1943/CH4/EX4.4/Ex4_4.sce b/1943/CH4/EX4.4/Ex4_4.sce new file mode 100755 index 000000000..d4098f1d9 --- /dev/null +++ b/1943/CH4/EX4.4/Ex4_4.sce @@ -0,0 +1,51 @@ + +clc
+clear
+//Input data
+C=61;//The mass of carbon present in the coal according to coal analysis on mass basis in %
+H=4;//The mass of hydrogen present in the coal according to coal analysis on mass basis in %
+O=3;//The mass of oxygen present in the coal according to coal analysis on mass basis in %
+N=2;//The mass of nitrogen present in the coal according to coal analysis on mass basis in %
+S=1;//The mass of sulphur present in the coal according to coal analysis on mass basis in %
+M=4;//The mass of moisture present in the coal according to coal analysis on mass basis in %
+A=25;//The mass of ash present in the coal according to coal analysis on mass basis in %
+HHV=24.3;//The high heating value of the coal i.e energy released by complete combustion of 1 kg fuel in MJ/kg
+CO2=12;//The amount of carbondioxide by volume according to dry flue gas analysis in %
+CO=1.5;//The amount of carbonmonoxide by volume according to dry flue gas analysis in %
+O2=7;//The amount of oxygen by volume according to dry flue gas analysis in %
+N2=79.5;//The amount of nitrogen by volume according to dry flue gas analysis in %
+Te=170;//Exhaust gas temperature in degree centigrade
+L=0.03;//Energy loss other than dry exhaust loss and incomplete combustion is 3% of HHV
+R=150;//Steam generation rate in t/h
+Po=100;//Steam condition at boiler outlet in bar
+To=500;//Steam condition at boiler outlet in degree centigrade
+Ti=160;//Feed water inlet temperature in degree centigrade
+HCO2=33083;//Heat of reaction in kJ/kg carbon
+HCO=9500;//Heat of reaction in kJ/kg carbon
+cp=1.05;//Heat capacity of dry flue gas (dfg) in kJ/kgK
+Ta=30;//The ambient temperature of air in degree centigrade
+Mc=44;//Molecular weight of Carbondioxide
+Mco=28;//Molecular weight of carbonmonoxide
+Mo=32;//Molecular weight of oxygen
+Mn=28;//Molecular weight of nitrogen
+Mx=12;//Molecular weight of carbon
+h1=3373.7;//Enthalpy at 100 bar and 500 degree centigrade in kJ/kg
+hf=675.55;//Enthalpy at 160 degree centigrade in kJ/kg
+hg=2724.7;//Enthalpy at 100 bar in kJ/kg
+
+//Calculations
+Mdfg=([(C/100)*[(Mc*(CO2/100))+(Mco*(CO/100))+(Mo*(N2/100))]]/[Mx*[(CO2/100)+(CO/100)]]);//Mass of dry flue gas produced per kg of fuel in kg
+Ed=Mdfg*cp*(Te-Ta);//Energy loss due to dry exhaust gas in kJ/kg fuel
+//Since Mdfg is 11.73kg through sciab calculation, there is a variation in Ed value and Ei value
+Ei=[(Mdfg)*(HCO2-HCO)*(Mx/Mco)]*[(Mco*(CO/100))/[(Mc*(CO2/100))+(Mco*(CO/100))+(Mo*(O2/100))+(Mco*(N2/100))]];//Energy loss due to incomplete combustion in kJ/kg fuel
+El=L*HHV;//Energy loss other than dry exhaust loss and incomplete combustion loss in MJ/kg fuel
+TEl=(Ed/1000)+(Ei/1000)+El;//Total energy loss in MJ/kg fuel
+Be=[(HHV-TEl)/(HHV)]*100;//Boiler efficiency in %
+Wf=([(R*1000)*(h1-hf)]/((Be/100)*HHV*1000))/3600;//The fuel burning rate in kg/s
+Wth=(11.5*(C/100))+(34.5*[(H/100)-(O/800)])+(4.3*(S/100));//Thearetical air required per kg of fuel in kg
+WA=[[(3.04*(N2/100)*(C/100))]/[(CO2/100)+(CO/100)]]-[(N/100)*(1/0.768)];//Actual air supplied per kg of fuel in kg
+per=[(WA-Wth)/Wth]*100;//Percentage excess air used in %
+pea=[(h1-hg)/(h1-hf)]*100;//Percentage of energy absorbed in the superheater
+
+//Output
+printf('(a)The amount of dry flue gas produced per kg fuel = %3.2f kg \n (b)The dry exhaust loss = %3.1f kJ/kg fuel and incomplete combustion loss per kg fuel = %3.2f kJ/kg fuel \n (c)The boiler efficiency = %3.2f percentage \n (d) THe fuel burning rate = %3.3f kg/s \n (e)The percentage of excess air used = %3.2f percentage \n (f) The percentage of energy absorbed in the superheater = %3.2f percentage',Mdfg,Ed,Ei,Be,Wf,per,pea)
diff --git a/1943/CH4/EX4.5/Ex4_5.sce b/1943/CH4/EX4.5/Ex4_5.sce new file mode 100755 index 000000000..d809fa7d9 --- /dev/null +++ b/1943/CH4/EX4.5/Ex4_5.sce @@ -0,0 +1,34 @@ + +clc
+clear
+//Input data
+C=83.7;//The amount of carbon present in the fuel oil according to ultimate analysis of a fuel oil in %
+H=12.7;//The amount of hydrogen present in the fuel oil according to ultimate analysis of a fuel oil in %
+O=1.2;//The amount of oxygen present in the fuel oil according to ultimate analysis of a fuel oil in %
+N=1.7;//The amount of nitrogen present in the fuel oil according to ultimate analysis of a fuel oil in %
+S=0.7;//The amount of sulphur present in the fuel oil according to ultimate analysis of a fuel oil in %
+td=27;//The dry bulb temperature of combustion air in degree centigrade
+tw=21;//The wet bulb temperature of combustion air in degree centigrade
+E=0.3;//Excess air and assuming complete combustion in %
+t=200;//Temperature to find total volume of combustion products in degree centigrade
+p=1.013;//Pressure to find total volume of combustion procucts in bar
+
+//Calculations
+Wth=(11.5*(C/100))+[34.5*((H/100)-(O/100)*(1/8))]+(4.3*(S/100));//Theoretical air required per kg of fuel in kg
+WA=(1+E)*Wth;//Actual air required per kg of fuel in kg/kg fuel
+sh=0.0132;//Specific humidity at DBT and WBT in kg moisture/kg dry air
+W=WA*sh;//Water vapour entering with air per kg fuel in kg vap/kg fuel
+Tw=(9*(H/100))+WA;//Total water vapour formed per kg fuel in kg
+CO2=(44/12)*(C/100);//mass of carbondioxide gas per kg of fuel
+O2=0.232*E*Wth;//Mass of oxygen gas per kg of fuel
+N2=0.768*(1+E)*Wth+(N/100);//Mass of nitrogen gas per kg of fuel
+SO2=(64/32)*(S/100);//Mass of nitrogen gas per kg of fuel
+H2O=1.383;//Mass of water per kg of fuel
+M=(CO2/44)+(O2/32)+(N2/28)+(SO2/64)+(H2O/18);//Moles of combustion gases formed per kg fuel
+VG=M*22.4*[(273+t)/273]*(1.013/1.013);//Volume of flue gases at 200 degree centigrade and 1.013 bar per kg fuel
+CO21=((CO2/44)/[(CO2/44)+(O2/32)+(N2/28)])*100;//Composition of dry flue gas CO2 by volume
+O21=((O2/32)/[(CO2/44)+(O2/32)+(N2/28)])*100;//Composition of dry flue gas O2 by volume
+N21=((N2/28)/[(CO2/44)+(O2/32)+(N2/28)])*100;//Composition of dry flue gas N2 by volume
+
+//Output
+printf('(a)The total volume of combustion products at 200 degee centigrade and 1.013 bar = %3.2f m^3 \n (b)The dry flue gas analysis based on carbondioxide,oxygen and nitrogen is \n Carbondioxide = %3.2f percent \n Oxygen = %3.2f percent \n Nitrogen = %3.2f percent',VG,CO21,O21,N21)
diff --git a/1943/CH4/EX4.6/Ex4_6.sce b/1943/CH4/EX4.6/Ex4_6.sce new file mode 100755 index 000000000..dfacec0b8 --- /dev/null +++ b/1943/CH4/EX4.6/Ex4_6.sce @@ -0,0 +1,33 @@ + +clc
+clear
+//Input data
+C2H6=22.6;//The amount of gas present in the fuel gas according to volumetric analysis of fuel gas by volume in %
+CH4=73.6;//The amount of gas present in the fuel gas according to volumetric analysis of fuel gas by volume in %
+CO2=2.4;//The amount of gas present in the fuel gas according to volumetric analysis of fuel gas by volume in %
+N2=1.4;//The amount of gas present in the fuel gas according to volumetric analysis of fuel gas by volume in %
+E=0.25;//Assuming combustion air to be dry and in excess
+t=260;//The temperature for the total gas volume for complete combustion in degree centigrade
+p=1.013;//The pressure for the total gas volume for complete combustion in bar
+Mch=30;//Molecular weight of C2H6
+Mc=16;//Molecular weight of CH4
+Mco=44;//Molecular weight of CO2
+Mn=28;//Molecular weight of N2
+Mo=32;//Molecular weight of O2
+Mh=18;//Molecular weight of H2O
+
+//Calculations
+x=100;//Assuming 100 moles of fuel gas
+Mf=[(C2H6/100)*Mch]+[(CH4/100)*Mc]+[(N2/100)*Mn]+[(CO2/100)*Mco];//Molecular weight of fuel gas
+Ma=[(226.3*(Mo+(3.76*Mn))*(1+E))]/28.96;//Moles of air supplied
+Mc=1440;//Moles of combustion gas from the equation
+Mr=x+Ma+Mc;//Total reaction molecules
+Mwc=[(121.2*Mco)+(215*Mh)+(56.6*Mo)+(1065.4*Mn)]/Mc;//Molecular weight of combustion gas in kg/kgmol
+Mt=Mc/(x*20);//Total number of moles of combustion gas per kg fuel gas
+VG=Mt*22.4*[(273+t)/273];//Volume of combustion products per kg fuel gas
+CO21=(121.2/(121.2+56.6+1065.4))*100;//Gas analysis of CO2 by volume
+O21=(56.6/1243.2)*100;//Gas analysis of O2 by volume
+N2=(1065.4/1243.2)*100;//Gas analysis of N2 by volume
+
+//Output
+printf('(a)The molecular weight of the combustion products M = %3.2f kg/kg mol \n (b) The total gas volume for complete combustion at 260 degree centigrade and 1.013 bar is %3.2f m^3/kg fuel \n (c)The dry flue gas analysis on \n carbondioxide = %3.1f percent \n oxygen = %3.1f percent \n nitrogen = %3.1f percent ',Mwc,VG,CO21,O21,N2)
diff --git a/1943/CH4/EX4.7/Ex4_7.sce b/1943/CH4/EX4.7/Ex4_7.sce new file mode 100755 index 000000000..cc1cdd3d6 --- /dev/null +++ b/1943/CH4/EX4.7/Ex4_7.sce @@ -0,0 +1,19 @@ + +clc
+clear
+//Input data
+CO21=9.7;//Carbondioxide gas analysis before the air preheater
+CO22=9.2;//Carbondioxide gas analysis after the air preheater
+O21=4.0;//Oxygen gas analysis before the air preheater
+O22=4.9;//Oxygen gas analysis after the air preheater
+N21=86.3;//Nitrogen gas analysis before the air preheater
+N22=85.9;//Nitrogen gas analysis after the air preheater
+C=72;//The coal used shows the carbon percentage by mass in %
+
+//Calculations
+W1=[(3.04)*(N21/100)*(C/100)]/[(CO21/100)];//Before air preheater in kg air/kg fuel
+W2=[(3.04)*(N22/100)*(C/100)]/[(CO22/100)];//After air preheater in kg air/kg fuel
+A=W2-W1;//Air leakage in kg air/kg fuel
+
+//Output
+printf('The air leakage into the air preheater per kg of coal fired is %3.0f kg air/kg fuel',A)
diff --git a/1943/CH4/EX4.8/Ex4_8.sce b/1943/CH4/EX4.8/Ex4_8.sce new file mode 100755 index 000000000..65f3383a4 --- /dev/null +++ b/1943/CH4/EX4.8/Ex4_8.sce @@ -0,0 +1,31 @@ + +clc
+clear
+//Input data
+n=6;//Total lancashire boilers in a textile factory
+Ws=6;//Each boiler supplying steam in t/h
+p=16;//Pressure at which steam is supplied in bar
+t=250;//Temperature at which steam is supplied in degree centigrade
+CV=43960;//Calorific value of the fuel oil in kJ/kg
+no=75;//Overall efficiency of the boiler in %
+a=16;//The amount of air required for efficient burning of the fuel inkg
+H=20;//Drought of water gauge required at the base of chimney in mm
+tf=320;//The flue gases leave the boiler in degree centigrade
+ts=300;//The average temperature of the gases in the stack in degree centigrade
+ta=30;//The atmospheric temperature in degree centigrade
+R=0.287;//Real Gas constant in kJ/kgK
+h1=2919.2;//enthalpy at the entrance of the boiler in kJ/kgK
+hf=125.8;//Enthalpy at the feed in kJ/kgK
+pi=3.1412;//Mathematical constant
+g=9.81;//gravitational fore constant in m/s^2
+P=1.013;//Atmospheric pressure in bar
+
+//Calculations
+H1=[(H*R*(273+ta)*(273+ts))]/[P*100*[(273+ts)-(273+ta)]];//The draught produced in m
+Wf=[[(Ws*1000)*6*(h1-hf)]/((no/100)*CV)]/3600;//Air fuel ratio in kg/s
+Wa=a*Wf;//Actual air fuel ratio in kg/s
+Wfg=17*Wf;//Air fuel ratio in kg/s
+D=[[(Wfg*R*(273+ts)*(4/pi))]/[(101.3)*(2*g*H1)^(1/2)]]^(1/2);//Diameter at its base in m
+
+//Output
+printf('(a)The height of the stack H = %3.2f m \n (b)The diameter at its base D = %3.2f m ',H1,D)
diff --git a/1943/CH4/EX4.9/Ex4_9.sce b/1943/CH4/EX4.9/Ex4_9.sce new file mode 100755 index 000000000..83570f703 --- /dev/null +++ b/1943/CH4/EX4.9/Ex4_9.sce @@ -0,0 +1,27 @@ + +clc
+clear
+//Input data
+Wf=10;//Coal rate in t/h
+C=78;//The mass of carbon present in the coal according to coal analysis on mass basis in %
+H=3;//The mass of hydrogen present in the coal according to coal analysis on mass basis in %
+O=3;//The mass of oxygen present in the coal according to coal analysis on mass basis in %
+S=1;//The mass of sulphur present in the coal according to coal analysis on mass basis in %
+M=7;//The mass of moisture present in the coal according to coal analysis on mass basis in %
+A=8;//The mass of ash present in the coal according to coal analysis on mass basis in %
+E=0.3;//Excess air in percentage
+p=180;//Plenum chamber pressure in mm water gauge
+nm=0.6;//Mechanical efficiency of the fan
+ta=30;//Room temperature in degree centigrade
+R=0.287;//Real gas constant
+P=101.325;//Atmospheric pressure in kPa
+g=9.812;//gravitational force constant m/s^2
+
+//Calculations
+Wth=(11.5*(C/100))+(34.5*[(H/100)-(O/(8*100))])+(4.3*(S/100));//Theoretical air required per kg fuel in kg air/kg fuel
+WA=Wth*(1+0.3);//Actual air required per kg fuel in kg air/kg fuel
+Va=(R*(273+ta))/P;//Volume flow rate of air in m^3/kg
+FD=((WA*Wf*1000*Va*p*g)/(3600*nm))/1000;//FD fan motor capacity in kW
+
+//Output
+printf('The required motor capacity needed for the FD fan is %3.2f kW ',FD)
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