FE Chemical exam practice: cram pack

Formula sheets, the key method steps for every topic and 24 practice problems, with full solutions at the back.

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1Formulas and methods

Mass balance

Steady state
in = out
Total balance
ṁ1 + ṁ2 = ṁ3
Component balance
ṁ1x1 + ṁ2x2 = ṁ3x3
Evaporator
F·xF = P·xP, W = F − P

Energy balance

Sensible heat
Q = ṁ·cp·ΔT
Latent heat
Q = ṁ·hfg
Mixing
ΣṁcpTin = ΣṁcpTout
Water
cp ≈ 4.18 kJ/(kg·K)

Ideal gas law

Ideal gas law
pV = nRT
Gas constant
R = 8.314 J/(mol·K)
Combined gas law
p1V1/T1 = p2V2/T2
Moles
n = m/M
Temperature
T[K] = T[°C] + 273.15

Stoichiometry

Moles
n = m/M
Concentration
c = n/V
Mole ratio
use the coefficients of the balanced equation
Limiting reactant
the one that runs out first
Percent yield
actual / theoretical × 100%

Method

  1. Write and balance the chemical equation.
  2. Convert the given mass to moles: n = m/M.
  3. Use the coefficients as the mole ratio to find the moles of the substance you want.
  4. Convert back to mass with m = n·M. With two reactants, find the limiting reactant first.

Chemical equilibrium

Equilibrium constant
Kc = [C]c[D]d/([A]a[B]b)
ICE table
Initial, Change (×coefficient), Equilibrium
Quadratic
x = (−b + √(b² − 4ac))/(2a)

Method

  1. Write Kc with products over reactants, each raised to the power of its coefficient.
  2. Set up an ICE table: Initial, Change (in steps of x times the coefficients), Equilibrium.
  3. Put the equilibrium expressions into Kc and solve for x.
  4. Check whether x is small enough for an approximation; otherwise solve the quadratic.

Calorimetry & enthalpy

Heat
q = m·c·ΔT
Water
c = 4.18 J/(g·°C)
Calorimeter
heat lost = heat gained
Enthalpy of reaction
ΔH° = ΣΔH°f(products) − ΣΔH°f(reactants)

Reaction kinetics

First order
ln(CA/CA0) = −kt
Half-life (first order)
t½ = ln 2/k
Second order
1/CA = 1/CA0 + kt
Arrhenius
k = A·e−Ea/(RT)
Two temperatures
ln(k2/k1) = (Ea/R)(1/T1 − 1/T2)

Reactor sizing (CSTR & PFR)

Space time
τ = V/Q
CSTR, first order
τ = X/(k·(1 − X)), CA = CA0/(1 + kτ)
PFR, first order
τ = ln(1/(1 − X))/k, CA = CA0·e−kτ
Conversion from volume
CSTR: X = kτ/(1 + kτ), PFR: X = 1 − e−kτ
N equal CSTRs in series
X = 1 − 1/(1 + kτi)N

Heat exchangers (LMTD)

Heat duty
Q = U·A·ΔTlm
Log mean temperature difference
ΔTlm = (ΔT1 − ΔT2)/ln(ΔT1/ΔT2)
Stream balance
Q = ṁcp(Tin − Tout)

Heat conduction

Fourier’s law
Q̇ = kAΔT/L
Conduction resistance
R = L/(kA)
Convection resistance
R = 1/(hA)
Resistances in series
Q̇ = ΔTtotal/ΣR
U-value
U = 1/(ΣR·A)

Pipe friction & head loss

Reynolds number
Re = V·D/ν = ρ·V·D/μ
Flow regime
laminar below Re ≈ 2000, turbulent above Re ≈ 4000
Mean velocity
V = Q/A, A = π·D²/4
Darcy–Weisbach
hf = f·(L/D)·V²/(2g)
Minor losses
hm = ΣK·V²/(2g)
Typical K values
entrance 0.5, exit 1.0, 90° bend ≈ 0.3
Pressure drop
Δp = ρ·g·hf
Two open reservoirs
Δz = (f·L/D + ΣK)·V²/(2g)
Free outlet
H = (1 + f·L/D + ΣK)·V²/(2g)

Pumps & pump power

Hydraulic power
Ph = ρ·g·Q·H = Q·Δp
Shaft power
Pshaft = Ph/ηpump
Electrical power
Pel = Pshaft/ηmotor
Pump head
H = Δz + Δp/(ρ·g) + hL
System losses
hL = (f·L/D + ΣK)·V²/(2g)

2Practice problems

1.Mass balanceMedium
MixerStream 1350 kg/h · 50% NaOHStream 2ṁ₂ = ? · 10% NaOHProduct25% NaOH

How much of stream 2 must be added each hour to stream 1 so that the blended product contains 25% NaOH? Find ṁ2.

ṁ1 = 350 kg/hx1 = 50 %x2 = 10 %x3 = 25 %
ṁ2 = kg/h
2.Mass balanceHard
EvaporatorFeed F2400 kg/h · 12% sugarProduct P65% sugarVapour W (pure water)W = ? kg/h

An evaporator concentrates a sugar solution by boiling off pure water. Find the water evaporated W in kg/h.

F = 2400 kg/hxF = 12 %xP = 65 %
W = kg/h
3.Energy balanceMedium
hot sidecold sidelight oil · 150 °C90 °Cwater · 20 °Ct = ? °C

Hot light oil cools water in a counter-flow heat exchanger with no heat loss. Find the water outlet temperature tout.

ṁh = 2 kg/scp,h = 2.1 kJ/(kg·K)Th: 150 → 90 °Cṁc = 2 kg/scp,c = 4.18 kJ/(kg·K)tin = 20 °C
tout = °C
4.Energy balanceHard
hot sidecold sideglycol mix · 170 °C100 °Cwater · 20 °C85 °C · ṁ = ?5% lost

Hot glycol mix heats water in an exchanger that loses 5% of the heat released by the hot stream to the surroundings. Find the water flow rate ṁc needed.

ṁh = 2.5 kg/scp,h = 3.6 kJ/(kg·K)Th: 170 → 100 °Ct: 20 → 85 °Ccp,c = 4.18 kJ/(kg·K)loss = 5 %
ṁc = kg/s
5.Ideal gas lawMedium
370 g of CH₄P = 300 kPaT = 45 °CV = ?

What volume V does 370 g of CH₄ occupy at 300 kPa and 45 °C? Treat it as an ideal gas.

m = 370 gM = 16.04 g/molP = 300 kPaT = 45 °CR = 8.314 J/(mol·K)
V = L
6.Ideal gas lawHard
Ar, M = 39.95 g/molP = 750 kPaT = 40 °Cρ = ?

Find the density ρ of Ar at 750 kPa and 40 °C, treating it as an ideal gas.

M = 39.95 g/molP = 750 kPaT = 40 °CR = 8.314 J/(mol·K)
ρ = kg/m³
7.StoichiometryMedium
m(X)n(X)n(H2​O)m(H2​O)÷ M(X)× 4/ν× M(H2​O)

6 g of C3H8 and 48 g of O2 react according to C3H8 + 5O2 → 3CO2 + 4H2O. What mass m of H2O can form?

M(C3H8) = 44.1M(O2) = 32M(H2O) = 18.02 g/mol
m = g
8.StoichiometryHard
m(H2​)n(H2​)n(H2​O)m(H2​O)÷ M(H2​)× 2/2× M(H2​O)

In the reaction 2H2 + O2 → 2H2O, 4 g of H2 reacts completely (the other reactants are in excess) and 25.03 g of H2O is collected. Find the percent yield Y.

M(H2) = 2.016 g/molM(H2O) = 18.02 g/molactual: 25.03 g
Y = %
9.Chemical equilibriumMedium
H2​I2​HII0.80.80C−x−x+2xE0.8 − x0.8 − x2x

0.8 mol/L of H₂ and 0.8 mol/L of I₂ are put in a container and react: H₂ + I₂ ⇌ 2HI, with Kc = 64. Find the equilibrium concentration [HI].

[H₂]₀ = [I₂]₀ = 0.8 mol/LKc = 64
[HI] = mol/L
10.Chemical equilibriumHard
PCl5​PCl3​Cl2​I0.100C−x+x+xE0.1 − xxx

PCl₅ decomposes: PCl₅ ⇌ PCl₃ + Cl₂, with Kc = 0.2 at the reaction temperature. A container starts with 0.1 mol/L of PCl₅ only. Find the equilibrium concentration [PCl5].

[PCl₅]₀ = 0.1 mol/LKc = 0.2
[PCl5] = mol/L
11.Calorimetry & enthalpyMedium
Tf​ = ?Aluminiumm = 150 gT = 170 °Cc = 0.897 J/(g·°C)Waterm = 150 gT = 18 °Cc = 4.18 J/(g·°C)

A 150 g block of aluminium (c = 0.897 J/(g·°C)) at 170 °C is dropped into 150 g of water (c = 4.18 J/(g·°C)) at 18 °C in an insulated cup. Find the final temperature Tf.

mmetal = 150 gcmetal = 0.897 J/(g·°C)Tmetal = 170 °Cmwater = 150 gTwater = 18 °Ccwater = 4.18 J/(g·°C)
Tf = °C
12.Calorimetry & enthalpyHard
H250 g C3​H8​C3​H8​ + 5O₂reactants3CO₂ + 4H₂O(l)productsq = ?

Use the standard enthalpies of formation to find the heat q released when 250 g of C3H8 (M = 44.1 g/mol) burns completely: C3H8 + 5O₂ → 3CO₂ + 4H₂O(l). Give q as a positive number.

ΔH°f(C3H8) = −103.8 kJ/molΔH°f(CO₂) = −393.5 kJ/molΔH°f(H₂O, l) = −285.8 kJ/molΔH°f(O₂) = 0
q = kJ
13.Reaction kineticsMedium
t (min)X (%)t = ?50%

A zero-order reaction has k = 0.025 mol/(L·min) and starts at 2 mol/L. How long does it take to reach 50% conversion? Find t.

k = 0.025 mol/(L·min)CA0 = 2 mol/LX = 50 %
t = min
14.Reaction kineticsHard
Tk20 °C0.0140 °C?

A reaction has a rate constant of 0.01 min⁻¹ at 20 °C and an activation energy of 50 kJ/mol. Find the rate constant k2 at 40 °C.

k1 = 0.01 min⁻¹T1 = 20 °CT2 = 40 °CEa = 50 kJ/molR = 8.314 J/(mol·K)
k2 = min⁻¹
15.Reactor sizing (CSTR & PFR)Medium
QX = 85%same Q, k and X as the CSTR

A first-order liquid-phase reaction must reach 85% conversion. How many times larger must a CSTR be than a PFR for the same feed rate, rate constant and conversion? Find the ratio VCSTR/VPFR.

X = 85%first order, same k and Q
VCSTR/VPFR =
16.Reactor sizing (CSTR & PFR)Hard
V = 1000 LV = 1000 LQ = 50 L/minX = ?

A first-order liquid-phase reaction (k = 0.25 min⁻¹) runs in two equal CSTRs in series, each of 1000 L. The feed rate is 50 L/min, the density is constant and the reactors are at steady state. Find the overall conversion X in percent.

V = 1000 L (×2)Q = 50 L/mink = 0.25 min⁻¹
X = %
17.Heat exchangers (LMTD)Medium
lengthT150 °C100 °C140 °C25 °CΔT₁ΔT₂counter-flow

A shell-and-tube heat exchanger (one shell pass, two tube passes) must transfer 130 kW. The hot fluid cools from 150 to 100 °C and the cold fluid heats from 25 to 140 °C. The LMTD correction factor for this arrangement is F = 0.8, and U = 500 W/(m²·K). Find the heat transfer area A needed.

Q̇ = 130 kWF = 0.8U = 500 W/(m²·K)Th: 150 → 100 °CTc: 25 → 140 °C
A = m²
18.Heat exchangers (LMTD)Hard
lengthT150 °C85 °C?25 °CΔT₁ΔT₂counter-flow

In a counter-flow double-pipe heat exchanger, hot oil (1 kg/s, cp = 2.1 kJ/(kg·K)) flows in the inner tube and cools from 150 to 85 °C. Water (0.3 kg/s, cp = 4.18 kJ/(kg·K)) in the annulus enters at 25 °C. The inner tube has a diameter of 32 mm, and U = 500 W/(m²·K) is based on this diameter. Find the tube length L needed.

ṁh = 1 kg/scp,h = 2.1 kJ/(kg·K)Th: 150 → 85 °Cṁc = 0.3 kg/sTc,in = 25 °CD = 32 mmU = 500 W/(m²·K)
L = m
19.Heat conductionMedium
Brick, k = 0.72250 mmConcrete, k = 1.4100 mm15 °C9 °CTi​ = ?Q̇

A wall is made of 250 mm of brick and 100 mm of concrete, with an area of 6 m². The outer faces are at 15 °C and 9 °C. Find the temperature Ti at the interface between the two layers.

L1 = 250 mm, k1 = 0.72 W/(m·K)L2 = 100 mm, k2 = 1.4 W/(m·K)A = 6 m²T1 = 15 °CT3 = 9 °C
Ti = °C
20.Heat conductionHard
Expanded polystyrene, k = 0.035200 mmGlass, k = 0.96150 mmroom 20 °Coutside -8 °CQ̇ = ?

A wall of 200 mm expanded polystyrene and 150 mm glass separates a room at 20 °C from outside air at -8 °C. The convection coefficients are 8 W/(m²·K) inside and 20 W/(m²·K) outside, and the wall area is 20 m². Find the heat loss Q̇ through the wall.

L1 = 200 mm, k1 = 0.035 W/(m·K)L2 = 150 mm, k2 = 0.96 W/(m·K)A = 20 m²hi = 8 W/(m²·K)ho = 20 W/(m²·K)Troom = 20 °CTout = -8 °C
Q̇ = W
21.Pipe friction & head lossMedium
V = 0.8 m/sD = 50 mmL = 300 mf = 0.018

Water flows at a mean velocity of 0.8 m/s through a pipe 300 m long with an inside diameter of 50 mm. Use the Darcy friction factor f = 0.018 and g = 9.81 m/s². Find the friction head loss hf.

V = 0.8 m/sL = 300 mD = 50 mmf = 0.018g = 9.81 m/s²
hf = m
22.Pipe friction & head lossHard
K = 0.2Δz = 6 mL = 200 m, D = 200 mm, f = 0.0154× bend (K = 0.3)

Two open reservoirs are joined by a pipe 200 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.015. The water surface of the upper reservoir is 6 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 4 bends (K = 0.3 each), a valve (K = 0.2) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². Find the flow rate Q in L/s.

Δz = 6 mL = 200 mD = 200 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 0.2Kexit = 1.0
Q = L/s
23.Pumps & pump powerMedium
PQ = 100 L/sH = 58 m

A pump with an efficiency of 72% delivers 100 L/s of water (ρ = 1000 kg/m³) against a head of 58 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 100 L/sH = 58 mη = 72%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 20 L/sΔz = 9 mL = 100 m, D = 100 mm, f = 0.018, ΣK = 3

A pump moves 20 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 9 m higher. The pipe is 100 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 3 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 78%. Find the shaft power Pshaft in kW.

Q = 20 L/sΔz = 9 mL = 100 mD = 100 mmf = 0.018ΣK = 3η = 78%
Pshaft = kW

3Solutions

1.Mass balance

Answer: ṁ2 = 583.3 kg/h

Steady-state mass balance: in = out for the total and for each component. Blending problems combine both.

Balances

Total: ṁ3 = ṁ1 + ṁ2
NaOH: ṁ1x1 + ṁ2x2 = (ṁ1 + ṁ2)x3

Solve for ṁ2

ṁ2 = ṁ1(x1 − x3)/(x3 − x2) = 350·(50 − 25)/(25 − 10) = 583.3 kg/h

Answer

ṁ2 = 583.3 kg/h
2.Mass balance

Answer: W = 1957 kg/h

Tie component: a component that passes through unchanged in one stream (here the solute) links the flows directly. Then the total balance gives the rest.

Solute balance

F·xF = P·xP → P = 2400·12/65 = 443.1 kg/h

Total balance

W = F − P = 2400 − 443.1 = 1957 kg/h

Answer

W = 1957 kg/h
3.Energy balance

Answer: tout = 50.14 °C

Exchanger energy balance: with no losses, ṁhcp,h(Th,in − Th,out) = ṁccp,c(tout − tin).

Heat released by the hot stream

Q = 2·2.1·(150 − 90) = 252 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 20 + 252/(2·4.18) = 50.14 °C

Answer

tout = 50.14 °C
4.Energy balance

Answer: ṁc = 2.203 kg/s

Energy balance with losses: heat released = heat absorbed + heat lost.

Heat released

Qh = 2.5·3.6·(170 − 100) = 630 kW

Heat that reaches the water

Qc = (1 − 0.05)·630 = 598.5 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 598.5/(4.18·65) = 2.203 kg/s

Answer

ṁc = 2.203 kg/s
5.Ideal gas law

Answer: V = 203.4 L

Ideal gas law: PV = nRT, with n = m/M.

Moles

n = 370/16.04 = 23.07 mol
T = 45 + 273.15 = 318.1 K

Volume

V = nRT/P = 23.07·8.314·318.1/300 = 203.4 L

Answer

V = 203.4 L
6.Ideal gas law

Answer: ρ = 11.51 kg/m³

Ideal gas density: ρ = PM/(RT).

Rearrange the gas law

PV = (m/M)RT → ρ = m/V = PM/(RT)
T = 40 + 273.15 = 313.1 K

Density

ρ = 750·39.95/(8.314·313.1) = 11.51 kg/m³

Answer

ρ = 11.51 kg/m³
7.Stoichiometry

Answer: m = 9.807 g

Stoichiometry: a balanced equation counts particles, not grams. Convert mass to moles with n = m/M, use the coefficients of the equation as the mole ratio, then convert back with m = n·M. With two reactants, the limiting reactant is the one that runs out first and fixes how much product forms.

Moles of each reactant

n(C3H8) = 6/44.1 = 0.1361 mol
n(O2) = 48/32 = 1.5 mol

Limiting reactant

0.1361/1 = 0.1361, 1.5/5 = 0.3 → C3H8

Mass of product

n(H2O) = 0.1361·4 = 0.5442 mol
m = 0.5442·18.02 = 9.807 g

Answer

m = 9.807 g
8.Stoichiometry

Answer: Y = 70.01 %

Stoichiometry: a balanced equation counts particles, not grams. Convert mass to moles with n = m/M, use the coefficients of the equation as the mole ratio, then convert back with m = n·M. With two reactants, the limiting reactant is the one that runs out first and fixes how much product forms.

Theoretical yield

n(H2) = 4/2.016 = 1.984 mol
m = 1.984·2/2·18.02 = 35.75 g

Percent yield

Y = 25.03/35.75·100 = 70.01%

Answer

Y = 70.01%
9.Chemical equilibrium

Answer: [HI] = 1.28 mol/L

Chemical equilibrium: for aA + bB ⇌ cC + dD, the equilibrium constant is Kc = [C]c[D]d/([A]a[B]b), using concentrations at equilibrium. An ICE table (Initial, Change, Equilibrium) links the starting amounts to the equilibrium amounts through one unknown x, scaled by the coefficients.

Equilibrium expression

64 = (2x)²/(0.8 − x)²

Take the square root

8 = 2x/(0.8 − x) → x = 0.8·8/(2 + 8) = 0.64 mol/L

Equilibrium concentration

[HI] = 2x = 1.28 mol/L

Answer

[HI] = 1.28 mol/L
10.Chemical equilibrium

Answer: [PCl5] = 0.02679 mol/L

Chemical equilibrium: for aA + bB ⇌ cC + dD, the equilibrium constant is Kc = [C]c[D]d/([A]a[B]b), using concentrations at equilibrium. An ICE table (Initial, Change, Equilibrium) links the starting amounts to the equilibrium amounts through one unknown x, scaled by the coefficients.

Equilibrium expression

0.2 = x²/(0.1 − x) → x² + 0.2·x − 0.02 = 0

Solve the quadratic

x = (−0.2 + √(0.2² + 4·0.02))/2 = 0.07321 mol/L

Equilibrium concentration

[PCl₅] = 0.1 − 0.07321 = 0.02679 mol/L

Answer

[PCl5] = 0.02679 mol/L
11.Calorimetry & enthalpy

Answer: Tf = 44.86 °C

Heat and enthalpy: heating a substance takes q = m·c·ΔT. In a calorimeter the heat lost by the hot object equals the heat gained by the cold one. The enthalpy change of a reaction follows from enthalpies of formation: ΔH° = ΣΔH°f(products) − ΣΔH°f(reactants), each multiplied by its coefficient.

Heat balance

150·0.897·(170 − Tf) = 150·4.18·(Tf − 18)

Solve for the final temperature

Tf = (134.6·170 + 627·18)/(134.6 + 627) = 44.86 °C

Answer

Tf = 44.86 °C
12.Calorimetry & enthalpy

Answer: q = 12584 kJ

Heat and enthalpy: heating a substance takes q = m·c·ΔT. In a calorimeter the heat lost by the hot object equals the heat gained by the cold one. The enthalpy change of a reaction follows from enthalpies of formation: ΔH° = ΣΔH°f(products) − ΣΔH°f(reactants), each multiplied by its coefficient.

Enthalpy of reaction

ΔH° = [3·(−393.5) + 4·(−285.8)] − [1·(−103.8) + 5·0] = −2220 kJ

Heat for the given mass

n = 250/44.1 = 5.669 mol
q = n·|ΔH°/1| = 5.669·2220 = 12584 kJ

Answer

q = 12584 kJ
13.Reaction kinetics

Answer: t = 40 min

Integrated rate laws: zero order: C = C₀ − kt (straight line, t½ = C₀/(2k)); first order: ln(C₀/C) = kt (t½ = ln 2/k); second order: 1/C − 1/C₀ = kt (t½ = 1/(kC₀)). Conversion X means C = C₀(1 − X).

Amount converted

CA0·X = 2·0.5 = 1 mol/L

Time

t = CA0·X/k = 1/0.025 = 40 min

Answer

t = 40 min
14.Reaction kinetics

Answer: k2 = 0.03707 min⁻¹

Reaction rates: for a first-order reaction −dC/dt = kC, so C = C₀·e−kt and the half-life ln 2/k does not depend on concentration. For a second-order reaction 1/C = 1/C₀ + kt. The rate constant rises with temperature following Arrhenius: k = A·e−Ea/(RT).

Absolute temperatures

T1 = 293.1 K, T2 = 313.1 K

Arrhenius ratio

ln(k2/k1) = −(50000/8.314)·(1/313.1 − 1/293.1) = 1.31
k2 = 0.01·e1.31 = 0.03707 min⁻¹

Answer

k2 = 0.03707 min⁻¹
15.Reactor sizing (CSTR & PFR)

Answer: VCSTR/VPFR = 2.987

Ideal reactors, first-order reaction (−rA = k·CA) at steady state, with space time τ = V/Q. A CSTR is perfectly mixed, so the whole volume reacts at the low outlet concentration: τ = X/(k·(1 − X)) and CA = CA0/(1 + k·τ). In a PFR each slice of fluid reacts like a small batch reactor: τ = ln(1/(1 − X))/k and CA = CA0·e−k·τ. For the same conversion a CSTR always needs more volume than a PFR.

k·τ for each reactor

CSTR: k·τ = X/(1 − X) = 0.85/0.15 = 5.667
PFR: k·τ = ln(1/(1 − X)) = ln(6.667) = 1.897

Ratio of volumes

VCSTR/VPFR = 5.667/1.897 = 2.987

Answer

VCSTR/VPFR = 2.987

The gap grows quickly at high conversion.

16.Reactor sizing (CSTR & PFR)

Answer: X = 97.22 %

Ideal reactors, first-order reaction (−rA = k·CA) at steady state, with space time τ = V/Q. A CSTR is perfectly mixed, so the whole volume reacts at the low outlet concentration: τ = X/(k·(1 − X)) and CA = CA0/(1 + k·τ). In a PFR each slice of fluid reacts like a small batch reactor: τ = ln(1/(1 − X))/k and CA = CA0·e−k·τ. For the same conversion a CSTR always needs more volume than a PFR.

Space time

τ = V/Q = 1000/50 = 20 min, kτ = 0.25·20 = 5

Conversion

C1/CA0 = 1/(1 + kτ) = 1/(1 + 5) = 0.1667
C2/CA0 = 1/(1 + kτ)² = 0.02778
X = 1 − 0.02778 = 97.22%

Answer

X = 97.22%
17.Heat exchangers (LMTD)

Answer: A = 10.07 m²

LMTD method: the temperature difference between the streams changes along the exchanger, so the rate equation uses its logarithmic mean: Q̇ = U·A·ΔTlm, with ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂), where ΔT₁ and ΔT₂ are the differences at the two ends. Counter-flow gives a larger ΔTlm than parallel flow for the same inlet and outlet temperatures.

End temperature differences (counter-flow)

In counter-flow the hot inlet faces the cold outlet, and the hot outlet faces the cold inlet.

ΔT₁ = Th,in − Tc,out = 150 − 140 = 10 K
ΔT₂ = Th,out − Tc,in = 100 − 25 = 75 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (10 − 75)/ln(10/75) = 32.26 K

Area

A = Q̇/(U·F·ΔTlm,cf) = 130000/(500·0.8·32.26) = 10.07 m²

Answer

A = 10.07 m²
18.Heat exchangers (LMTD)

Answer: L = 81.28 m

LMTD method: the temperature difference between the streams changes along the exchanger, so the rate equation uses its logarithmic mean: Q̇ = U·A·ΔTlm, with ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂), where ΔT₁ and ΔT₂ are the differences at the two ends. Counter-flow gives a larger ΔTlm than parallel flow for the same inlet and outlet temperatures.

Heat duty and water outlet temperature

Q̇ = 1·2.1·(150 − 85) = 136.5 kW
Tc,out = 25 + 136.5/(0.3·4.18) = 133.9 °C

End temperature differences

In counter-flow the hot inlet faces the cold outlet, and the hot outlet faces the cold inlet.

ΔT₁ = Th,in − Tc,out = 150 − 133.9 = 16.15 K
ΔT₂ = Th,out − Tc,in = 85 − 25 = 60 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (16.15 − 60)/ln(16.15/60) = 33.41 K

Area and length

A = 136500/(500·33.41) = 8.171 m²
L = A/(πD) = 8.171/(π·0.032) = 81.28 m

Answer

L = 81.28 m
19.Heat conduction

Answer: Ti = 10.02 °C

Thermal resistance: steady heat flow through layers in series behaves like current through resistors in series: Q̇ = ΔT/ΣR, with R = L/(kA) for a conducting layer and R = 1/(hA) for a convecting surface. The temperature drop across each layer is proportional to its resistance.

Layer resistances

R1 = L1/(k1A) = (250/1000)/(0.72·6) = 0.05787 K/W
R2 = L2/(k2A) = (100/1000)/(1.4·6) = 0.0119 K/W

Heat flow

Q̇ = (T1 − T3)/(R1 + R2) = 6/0.06978 = 85.99 W

Interface temperature

The temperature drops across the first layer by Q̇·R₁.

Ti = T1 − Q̇·R1 = 15 − 85.99·0.05787 = 10.02 °C

Answer

Ti = 10.02 °C
20.Heat conduction

Answer: Q̇ = 92.63 W

Thermal resistance: steady heat flow through layers in series behaves like current through resistors in series: Q̇ = ΔT/ΣR, with R = L/(kA) for a conducting layer and R = 1/(hA) for a convecting surface. The temperature drop across each layer is proportional to its resistance.

Resistances in series

Ri = 1/(hiA) = 1/(8·20) = 0.00625 K/W
R1 = L1/(k1A) = (200/1000)/(0.035·20) = 0.2857 K/W
R2 = L2/(k2A) = (150/1000)/(0.96·20) = 0.007813 K/W
Ro = 1/(hoA) = 1/(20·20) = 0.0025 K/W
ΣR = 0.3023 K/W

Heat loss

Q̇ = (20 − (-8))/0.3023 = 92.63 W

Answer

Q̇ = 92.63 W
21.Pipe friction & head loss

Answer: hf = 3.523 m

Pipe flow: the Reynolds number Re = V·D/ν = ρ·V·D/μ tells laminar flow (Re below about 2000) from turbulent flow (above about 4000). Friction along a pipe costs the Darcy–Weisbach head loss hf = f·(L/D)·V²/(2g). Fittings, valves, the entrance and the exit add minor losses hm = ΣK·V²/(2g). Between two open reservoir surfaces the energy equation gives Δz = hf + hm, with the exit loss K = 1 included.

Velocity head

V²/(2g) = 0.8²/(2·9.81) = 0.03262 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.018·(300/0.05)·0.8²/(2·9.81) = 3.523 m

Answer

hf = 3.523 m
22.Pipe friction & head loss

Answer: Q = 80.57 L/s

Pipe flow: the Reynolds number Re = V·D/ν = ρ·V·D/μ tells laminar flow (Re below about 2000) from turbulent flow (above about 4000). Friction along a pipe costs the Darcy–Weisbach head loss hf = f·(L/D)·V²/(2g). Fittings, valves, the entrance and the exit add minor losses hm = ΣK·V²/(2g). Between two open reservoir surfaces the energy equation gives Δz = hf + hm, with the exit loss K = 1 included.

Loss coefficients

f·L/D = 0.015·200/0.2 = 15
ΣK = 0.5 + 4·0.3 + 0.2 + 1.0 = 2.9

Energy equation

Both surfaces are open to the air and practically at rest, so all of Δz is lost in the pipe.

6 = (15 + 2.9)·V²/(2·9.81)
V = √(2·9.81·6/17.9) = 2.564 m/s

Flow rate

Q = V·π·D²/4 = 2.564·0.03142 = 0.08057 m³/s = 80.57 L/s

Answer

Q = 80.57 L/s
23.Pumps & pump power

Answer: Pshaft = 79.03 kW

Pump power: the power given to the water is the hydraulic power Ph = ρ·g·Q·H = Q·Δp. The shaft must deliver more because the pump loses some: Pshaft = Ph/ηpump, and the motor draws Pel = Pshaft/ηmotor. The pump head H follows from the energy equation: static lift + pressure head + all friction and minor losses.

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.1·58 = 56.9 kW

Shaft power

Pshaft = Ph/η = 56.9/0.72 = 79.03 kW

Answer

Pshaft = 79.03 kW
24.Pumps & pump power

Answer: Pshaft = 4.01 kW

Pump power: the power given to the water is the hydraulic power Ph = ρ·g·Q·H = Q·Δp. The shaft must deliver more because the pump loses some: Pshaft = Ph/ηpump, and the motor draws Pel = Pshaft/ηmotor. The pump head H follows from the energy equation: static lift + pressure head + all friction and minor losses.

Velocity

V = Q/A = 0.02/0.007854 = 2.546 m/s
V²/(2g) = 0.3305 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (18 + 3)·0.3305 = 6.941 m

Pump head

H = Δz + hL = 9 + 6.941 = 15.94 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.02·15.94/0.78 = 4.01 kW

Answer

Pshaft = 4.01 kW

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