introduction to air pollution - workbook

10
CONVERSION OF UNITS Problem : An SO 2 concentration is given as 830mg/m 3 at 25°C and 1 atm. Express this concentration in parts per million (ppm). Solution : Step 1 Concentration of SO 2 is 830 mg/m 3 AT STP conditions (25°C and 1 atm), one mole of gas occupies 24.5 L (V=nRT/P). Molecular Weight of SO 2 is 64g/mol Step 2 ppm = concentration(10 mg/m 3 ) x 24.5 L/mol molecular weight(g/mol) x 1000 (mL/m 3 *g) Step 3 ppm = 830 (mg/m 3 ) x 24.5 L/mol 64 (g/1 mol SO 2 ) x 1000 (mL/m 3 *g) = 0.32 ppm Exercise: Carbon Monoxide concentration at 90°C and 6 atm is 90 mg/m 3 . Express this concentration in ppm. (0.016 ppm) Problem : The exhaust from a 1981 Honda contains 1.5% by volume of carbon monoxide. Compute the concentration of CO in milligrams/m 3 at 25°C and 1 atm of pressure. Solution : Step 1 1 percent by volume = 10 4 ppm. Introduction to Air Pollution - Workbook http://www.eng.utoledo.edu/~akumar/IAP1/aprg_remains/workbook/cha... 1 of 10 11/7/2012 5:00 PM

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Page 1: Introduction to Air Pollution - Workbook

CONVERSION OF UNITS

Problem :

An SO2 concentration is given as 830mg/m3 at 25°C and 1 atm. Express this concentration in parts per

million (ppm).

Solution :

Step 1

Concentration of SO2 is 830 mg/m3

AT STP conditions (25°C and 1 atm), one mole of gas occupies 24.5 L

(V=nRT/P).Molecular Weight of SO

2 is 64g/mol

Step 2

ppm =

concentration(10 mg/m3) x 24.5 L/mol

molecular weight(g/mol) x 1000 (mL/m3*g)

Step 3

ppm =

830 (mg/m3) x 24.5 L/mol

64 (g/1 mol SO2) x 1000 (mL/m3*g)

= 0.32 ppm

Exercise: Carbon Monoxide concentration at 90°C and 6 atm is 90 mg/m3. Express this concentration in ppm.(0.016 ppm)

Problem :The exhaust from a 1981 Honda contains 1.5% by volume of carbon monoxide. Compute the concentration

of CO in milligrams/m3 at 25°C and 1 atm of pressure.

Solution :

Step 1

1 percent by volume = 104 ppm.

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1.5 percent by volume = 1.5*104 ppm.Molecular Weight of CO is 28 g/mol

Step 2

concentration (mg/m3) =

ppm x molecular weight(g/mol) x 1000 (mg*L/m3*g)

24.5 (L/mol)

Step 3

concentration (mg/m3) =

1.5 x 104 ppm x 28(g/mol) x 1000 (mg*L/m3*g)

24.5 (L/mol)

= 1.71 x 107 ug/m3 = 1.71 x 104 mg/m3

Exercise: An exhaust gas containing 3.2 percent by volume SO2 is released at 25°C and 1 atm. Compute the

concentration in mg/m3.

(8.36 x 104 mg/m3)

Weight Fraction, Mole Fraction, and Average Molecular Weight

BASIC EQUATIONS :

Density : mass

volume

Specific gravity : density of a given substance

density of water =

density of a given substance

1 g/cm3

For example Specific gravity of methanol is given as 0.91. Therefore density of methanol is 0.91 multiplied

by density of water = 1 g/cm3.Supposing a mixture has A, B, and C as its components. Then,

Weight fraction of A = ( Wt. of A ) / ( Total Wt. )Mole fraction of A = ( Moles of A ) / ( Total moles )Number of moles of A = ( Wt. of A ) / ( Mol. Wt of A )Total Wt = Wt(A) + Wt(B) + Wt(C).Total moles = moles

A + moles

B + moles

C.

Problem :Determine the mole fraction, weight fraction and average molecular weight of all the components in a

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mixture, if contains 20 lbs of O2, 30 lbs of NO2 and 10 lbs of SO2.

Solution :Step 1Find the molecular weight(mol.wt.) of each gas.mol.wt. of O2 = 32g/mole.

mol.wt. of SO2 = 64g/mole.

mol.wt. of NO2 = 46g/mole.

Step 2Determine the number of moles of each gas.

moles of O2 = 20 lbs / (32g * 10-3kg/g * 2.2 lb/kg) = 284.1

moles. moles of NO2 = 30 lbs / (46g * 10-3kg/g * 2.2 lb/kg) = 296.4 moles.

moles of SO2 = 10 lbs / (64g * 10-3kg/g * 2.2 lb/kg) = 71 moles.

Total moles = 284.1 + 296.4 + 71 = 651.1.Step 3Determine mole fractions.mole fraction O

2 = 284.1 / 651.5. = 0.436.

mole fraction NO2 = 296.4 / 651.5. = 0.455.

mole fraction SO2 = 71.0 / 651.5 = 0.109.

Step 4Determine the weight fractions.Wt. fraction. O

2 = 20/(20+30+10) = 2/6.

Wt. fraction. NO2 = 30/60. = 1/2

Wt. fraction. SO2 = 10/60 = 1/6

Step5Determine the average mol.wt. of mixture.Average mol. wt. = (mol.wt of A * mole fraction of A) + (mol.wt of B * mole fraction of B) + (mol.wt of C *mole fraction of C).Avg. mol.wt. = 32*0.436 + 46*0.455+64 *0.109 = 41.858 g/mole.

Exercise: For a mixture equal weights of O2 and SO2, determine the mole fractions and weight fraction of

each component and the average molecular weight of the mixture.(O2: 0.67 mol frac., 0.5 weigh frac.;

SO2: 0.33 mol frac., 0.5 weigh frac.;

average molecular weight: 42.6 g/mol)

ATMOSPHERIC PRESSUREDefinition

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Atmospheric pressure is the pressure exerted by the atmosphere on the liquid surface. It

is equal to 101.3 KPa absolute (760mm of mercury or 2116 lbf/ft2).

Absolute pressure :Gage pressure + Atmospheric pressure.

Problem :Determine the pressure, both absolute and gauge, exerted at the bottom of the column of liquid, with 1mheight and with a density of 1200 Kg/m3.Solution :Pgage = Density*accel. due to gravity *height of liquid column. = 1200 Kg/m3 * 9.8 m/s2 * 1 m = 11.760 N/m2

Pabsolute = 101.3 + 11.760 = 113.06.KPa.

Exercise: Determine the absolute and gauge pressure exerted at the bottom of the column of liquid, with 11

meters high and with a density of 1 Kg/m3.(P

gauge = 0.107 kPa, P

absolute = 101.407 kPa)

GAS LAWFormula :

P V = n R Twhere,

P: Absolute PressureV : Volume occupied.T : Absolute temperature.n : Number of molesR : Gas law constant. = 1.986 cal/gmole-K.

Absolute temperatures ( Rankine or Kelvin) are used in the ideal gas law.Temperature in F + 460 = Temperature in Rankine.Temperature in C + 273 = Temperature in Kelvin.Rewriting ideal gas law in terms of density,Density = mass/volume = n * mol.wt. of gas / Volume.where,

n = number of moles = (P*V ) / ( R*T).Density = P*mol.wt. / ( R * T)By combining Boyle's law and Charles law, we get

{ q * P / T } a = { q * P / T} swhere,

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q :Volumetric flow rateP : Absolute pressure.T :Absolute temperature.s : Standard conditionsa : Actual conditions.

Problem :Calculate the density of a gas whose molecular weight is 29 at 1 atm,absolute and 80°F.Solution :80 F = 80 + 460 = 560 Rdensity = P * mol.wt/RTR = 0.73 atm-ft3 /lb mol-R.density = 1*29/0.73*540 = 0.0735 lb/ft3.

Exercise: Calculate the density of the same gas at 3 atm and 212°F

(0.1773 lb/ft3)

Problem :Determine the actual volumetric flow rate in acfm assuming that pressure is constant, when the actualtemperature is 700 F. The standard conditions are 70 F and 3000 cfm.Solution :Temperaturestd = 70 F = 530 R.

Temperatureact

= 700 F = 1160 R.

qact = qstd

*(Tempact /

Tempstd

).

= 3000*(1160 / 530). = 6566.03 acfm.

Exercise: Determine the actual volumetric flow rate of the above furnace's releases at 1 atm and 65°F.(3268.86 L/hr)

Problem :

For an SO2 emission of 22000 kg/day and an exhaust gas flow rate of 5.0 million m3/hr (after the scrubber)

measured at 150°C and 1 atm of pressure, calculate the concentration (ppm) of SO2 in the exhaust gases.

Solution:Step 1 :

n = 22000kg

dayx 1000

g

kgx

g-mol

64 g

= 343750g-mol

day

Step 2:

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VSO2 = nRT

P =

343750 (g*mol/day) x 0.08206 (L*atm/gmol*°K) x (150+273)°K

1 atm

= 11932037 L/day

Step 3:

Vexhaust gases

= (5.0 x 106 m3/hour x 1000L/m3 x 24 hours/1 day)

= 1.2 x 1011 L/day

Step 4:For 1 day,

total volume = 1.2 x 1011 L

volume of SO2 = 1.1932037 x 107 L

Concentration SO2 =

VSO2

Vexhaust gases

= 1.1932037 x 107 L

1.2 x 1011 Lx 106 ppm

= 99 ppm

Exercise: Calculate the concentration of SO2 if the above measurements were made at 400°C and 2.5 atm.

(63 ppm)

STACK DISCHARGE VELOCITYDefinition :Stack discharge velocity is the velocity at which the exhaust gas from the process is discharged to theatmosphere.Problem :Determine the stack discharge velocity at 320°F if the standard conditions for the exhaust are 2000 scfm,60°F and 1 atm. The diameter of the stack is found to be 1.2 ft.Solution:Actual volumetric flow rates are always used to calculate stack discharge velocity.Pstd/Pact is usually equal to 1 as the gas is discharged into the atmosphere.

Step 1 :Calculate the qactual

Formula :qact = qstd * {Tact*Tstd} at constant pressure.Tact = 320 + 460 = 780 RTstd = 60 + 460 = 520 Rqstd = 2000 scfm.qact = 2000 * 780/520. = 3000 acfm.

Step 2 :

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Calculate crossectional area of the stack.

A = PI* D2/4.

=Pi * 1.22/4. = 1.130 ft2

Step 3 :Calculate discharge velocity.Discharge vel. = q

act / A

= 3000 / 1.13 = 2654.86 ft / min. = 44.2 ft / sec.

Note : The velocity calculated in the above problem is average velocity.

Exercise: Determine the stack discharge velocity at 125°F for a 2.4 ft diameter stack with the same standardexhaust conditions.(8.3 ft/sec)

REYNOLDS NUMBER (Re)Definition :Reynolds Number is the ratio of the inertial forces to viscous forces acting on a fluid. It provides informationabout the flow behavior of the fluid, i.e. whether the flow is laminar or transitional. It is defined:

Re = D*V*r

m=

D*V

u

D = diameter of duct

V = average velocity of fluid

m = viscosity of fluid

r = density of fluid

u = kinematic viscosity of liquid

In general,

laminar flow Re < 2000

transition region 2000 < Re < 4000

turbulent flow Re > 4000

although this varies from case to case

Problem :Determine the Reynolds number and the flow behavior for a gas flowing through a 1.7 ft diameter duct at a

velocity of 25 ft/sec. The density of the gas is 0.075 lb/ft3 and the viscosity is 1.16 x 10-5 lb/ft-s.Solution:Step 1:

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Re = D*V*r

m=

1.7 ft x 25 ft/sec x 0.075 lb/ft3

1.16 x 10-5 lb/ft*sec

= 2.75 x 105

Step 2:

2.75 x 105 > 4000 therefore flow is turbulent

Exercise: At what velocity would the above gas need to achieve laminar flow through the duct?(0.18 ft/sec)

REQUIRED HEAT RATEThe amount of heat required to a fluid which undergoes a temperature change can be defined as follows:

heat transferred = mCpDT

where, m = mass of fluid

Cp = heat capacity of fluid

DT = change in temperature

Furthermore, the rate of heat transfer, Q, can be defined:

Q = mC

pDT

t

where, t = time

Problem :Determine the rate of heat transfer if the mass flow rate of the gas stream is 1400 lb/min, when thetemperature of the gas is raised from 200°F to 1000°F. Cp is given as 0.26 Btu/lb-°F.

Solution:

Q = 1400 lb x 0.26 Btu/lb-°F x (1000°F-200°F)

1 min

= 2.912 x 105 Btu/min

Exercise: What would be the heat transferred over a period of one hour and 15 minutes?

(2.184 x 107 Btu)

GROSS HEATING VALUE (HVG)

Definition :Gross heating value of a mixture is given the sum of the heating value of each component multiplied by thatcomponents mole fraction, or

HVG = S(xi)(HVi)

where, xi = mole fraction of ith component

HVi = heat value of ith component

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Problem :Determine the HVG of a mixture which comprises of N2, CH4 C2H6, C3H6, and C4H10 with respective mole

fractions of 0.0515, 0.811, 0.0967, 0.0351, and 0.0056. Use the following data

Gas HVG (Btu/s-ft3)

N2 0

CH4 1013

C2H6 1700

C3H

6 1920

C4H

10 3218

Solution:HV

G = S(x

i)(HV

i)

= (0.0515 x 0)+(0.811 x 1013)+(0.0967 x 1700)+(0.0351 x 1920)+(0.0056 x 3218)

= 1071.35 (Btu/s-ft3)

Exercise: Find the HVG for the mixture if there were no nitrogen present.

(1129.55 (BTU/s-ft3))

HENRY'S LAWDefinition :Henry's law states that the partial pressure of the solute in equilibrium in solution is proportional to molefraction

pg = H*x

g

where, pg = partial pressure of gas (atm.)

H = Henry's las constant (atm/mole fraction)

xg = mole fraction of gas in solution

(Note: H is a function of temperature)

For and ideal gas,

pg = yg*P

where, Pg = total pressure

yg = mole fraction of gas in gaseous mixture

Problem :Determine the maximum mole fraction of SO2 that can be dissolved in a solution to exert a partial pressure of

0.01 atm at 80°F. Henry's law constant = 510 atm/mole fraction @ 1 atm, 80°FSolution:

xg = P

g

H =

0.01 atm

510 (atm/mole fraction)

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= 1.96 x 10-5

Exercise: Find the pressure exerted by the solution when the mole fraction of SO2 is 1.0.

(510 atm)

Click here for more problems

Drop in your comments and suggestions to

Ashok Kumar, [email protected] Sud, [email protected]

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