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 1200 kg/h · 45% sugarStream 2ṁ₂ = ? · 5% sugarProduct35% sugar

How much of stream 2 must be added each hour to stream 1 so that the blended product contains 35% sugar? Find ṁ2.

ṁ1 = 200 kg/hx1 = 45 %x2 = 5 %x3 = 35 %
ṁ2 = kg/h
2.Mass balanceHard
EvaporatorFeed F2200 kg/h · 11% sugarProduct PP = ? · 55%Vapour W (pure water)0% sugar

An evaporator concentrates a sugar solution by boiling off pure water. Find the product flow P in kg/h.

F = 2200 kg/hxF = 11 %xP = 55 %
P = kg/h
3.Energy balanceMedium
hot sidecold sidelight oil · 130 °C100 °Cwater · 25 °Ct = ? °C

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

ṁh = 0.5 kg/scp,h = 2.1 kJ/(kg·K)Th: 130 → 100 °Cṁc = 1 kg/scp,c = 4.18 kJ/(kg·K)tin = 25 °C
tout = °C
4.Energy balanceHard
hot sidecold sideethanol · 150 °C90 °Cwater · 20 °C70 °C · ṁ = ?15% lost

Hot ethanol heats water in an exchanger that loses 15% of the heat released by the hot stream to the surroundings. Find the water flow rate ṁc needed.

ṁh = 2.5 kg/scp,h = 2.44 kJ/(kg·K)Th: 150 → 90 °Ct: 20 → 70 °Ccp,c = 4.18 kJ/(kg·K)loss = 15 %
ṁc = kg/s
5.Ideal gas lawMedium
260 g of CH₄V = 5 LT = 70 °CP = ?

A tank of 5 L contains 260 g of CH₄ at 70 °C. Treat it as an ideal gas and find the pressure P.

m = 260 gM = 16.04 g/molV = 5 LT = 70 °CR = 8.314 J/(mol·K)
P = kPa
6.Ideal gas lawHard
CH₄, M = 16.04 g/molP = 800 kPaT = 100 °Cρ = ?

Find the density ρ of CH₄ at 800 kPa and 100 °C, treating it as an ideal gas.

M = 16.04 g/molP = 800 kPaT = 100 °CR = 8.314 J/(mol·K)
ρ = kg/m³
7.StoichiometryMedium
m(X)n(X)n(NH3​)m(NH3​)÷ M(X)× 2/ν× M(NH3​)

30 g of N2 and 20 g of H2 react according to N2 + 3H2 → 2NH3. What mass m of NH3 can form?

M(N2) = 28.02M(H2) = 2.016M(NH3) = 17.03 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, 30 g of H2 reacts completely (the other reactants are in excess) and 219.9 g of H2O is collected. Find the percent yield Y.

M(H2) = 2.016 g/molM(H2O) = 18.02 g/molactual: 219.9 g
Y = %
9.Chemical equilibriumMedium
H2​I2​HII0.10.10C−x−x+2xE0.1 − x0.1 − x2x

0.1 mol/L of H₂ and 0.1 mol/L of I₂ are put in a container and react: H₂ + I₂ ⇌ 2HI, with Kc = 54. Find the equilibrium concentration [H2].

[H₂]₀ = [I₂]₀ = 0.1 mol/LKc = 54
[H2] = mol/L
10.Chemical equilibriumHard
PCl5​PCl3​Cl2​I0.800C−x+x+xE0.8 − xxx

PCl₅ decomposes: PCl₅ ⇌ PCl₃ + Cl₂, with Kc = 0.04 at the reaction temperature. A container starts with 0.8 mol/L of PCl₅ only. Find the equilibrium concentration [Cl2].

[PCl₅]₀ = 0.8 mol/LKc = 0.04
[Cl2] = mol/L
11.Calorimetry & enthalpyMedium
Tf​ = ?Copperm = 250 gT = 90 °Cc = 0.385 J/(g·°C)Waterm = 100 gT = 23 °Cc = 4.18 J/(g·°C)

A 250 g block of copper (c = 0.385 J/(g·°C)) at 90 °C is dropped into 100 g of water (c = 4.18 J/(g·°C)) at 23 °C in an insulated cup. Find the final temperature Tf.

mmetal = 250 gcmetal = 0.385 J/(g·°C)Tmetal = 90 °Cmwater = 100 gTwater = 23 °Ccwater = 4.18 J/(g·°C)
Tf = °C
12.Calorimetry & enthalpyHard
H20 g C3​H8​C3​H8​ + 5O₂reactants3CO₂ + 4H₂O(l)productsq = ?

Use the standard enthalpies of formation to find the heat q released when 20 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)C (mol/L)5 min0.7

In a first-order reaction the concentration of A falls from 2 mol/L to 0.7 mol/L in 5 min. Find the rate constant k.

CA0 = 2 mol/LCA = 0.7 mol/Lt = 5 min
k = min⁻¹
14.Reaction kineticsHard
t (min)X (%)15 minX = ?

A first-order reaction has k = 0.005 min⁻¹ at 20 °C and an activation energy of 50 kJ/mol. The batch reactor is now run at 40 °C for 15 min. Find the conversion X reached.

k1 = 0.005 min⁻¹T1 = 20 °CEa = 50 kJ/molT2 = 40 °Ct = 15 minR = 8.314 J/(mol·K)
X = %
15.Reactor sizing (CSTR & PFR)Medium
Q = 25 L/minX = 90%V = ?, k = 0.3 min⁻¹

A first-order liquid-phase reaction A → B with k = 0.3 min⁻¹ is carried out in a plug-flow reactor (PFR) fed at 25 L/min. The density is constant and the reactor is at steady state. Find the reactor volume V in litres for 90% conversion of A.

Q = 25 L/mink = 0.3 min⁻¹X = 90%
V = L
16.Reactor sizing (CSTR & PFR)Hard
Q = 100 L/minX = ?V = 500 L

A first-order liquid-phase reaction (k = 0.12 min⁻¹) runs in a 500 L plug-flow reactor (PFR) fed at 100 L/min. The density is constant and the reactor is at steady state. Find the conversion X in percent.

V = 500 LQ = 100 L/mink = 0.12 min⁻¹
X = %
17.Heat exchangers (LMTD)Medium
lengthT140 °C10 °C125 °CΔT₁ΔT₂condensing steam

In a condenser, steam condenses at a constant 140 °C on the outside of the tubes. Cooling water (4 kg/s, cp = 4.18 kJ/(kg·K)) flows through the tubes and heats from 10 to 125 °C. The overall heat transfer coefficient is 1000 W/(m²·K). Find the heat transfer area A needed.

Ts = 140 °Cṁ = 4 kg/scp = 4.18 kJ/(kg·K)Tc: 10 → 125 °CU = 1000 W/(m²·K)
A = m²
18.Heat exchangers (LMTD)Hard
lengthT125 °C55 °C?20 °CΔT₁ΔT₂counter-flow

In a counter-flow double-pipe heat exchanger, hot oil (0.8 kg/s, cp = 2.1 kJ/(kg·K)) flows in the inner tube and cools from 125 to 55 °C. Water (1 kg/s, cp = 4.18 kJ/(kg·K)) in the annulus enters at 20 °C. The inner tube has a diameter of 32 mm, and U = 200 W/(m²·K) is based on this diameter. Find the tube length L needed.

ṁh = 0.8 kg/scp,h = 2.1 kJ/(kg·K)Th: 125 → 55 °Cṁc = 1 kg/sTc,in = 20 °CD = 32 mmU = 200 W/(m²·K)
L = m
19.Heat conductionMedium
Gypsum board, k = 0.17250 mmMineral wool, k = 0.04150 mm23 °C10 °CTi​ = ?Q̇

A wall is made of 250 mm of gypsum board and 150 mm of mineral wool, with an area of 8 m². The outer faces are at 23 °C and 10 °C. Find the temperature Ti at the interface between the two layers.

L1 = 250 mm, k1 = 0.17 W/(m·K)L2 = 150 mm, k2 = 0.04 W/(m·K)A = 8 m²T1 = 23 °CT3 = 10 °C
Ti = °C
20.Heat conductionHard
Expanded polystyrene, k = 0.03550 mmBrick, k = 0.7275 mmroom 22 °Coutside -7 °CQ̇ = ?

A wall of 50 mm expanded polystyrene and 75 mm brick separates a room at 22 °C from outside air at -7 °C. The convection coefficients are 10 W/(m²·K) inside and 25 W/(m²·K) outside, and the wall area is 6 m². Find the heat loss Q̇ through the wall.

L1 = 50 mm, k1 = 0.035 W/(m·K)L2 = 75 mm, k2 = 0.72 W/(m·K)A = 6 m²hi = 10 W/(m²·K)ho = 25 W/(m²·K)Troom = 22 °CTout = -7 °C
Q̇ = W
21.Pipe friction & head lossMedium
V = 2.8 m/sD = 300 mmL = 100 mf = 0.025

Water (ρ = 1000 kg/m³) flows at 2.8 m/s through a horizontal pipe, 100 m long, with an inside diameter of 300 mm. Use the Darcy friction factor f = 0.025 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 2.8 m/sL = 100 mD = 300 mmf = 0.025ρ = 1000 kg/m³
Δp = kPa
22.Pipe friction & head lossHard
K = 0.2free outletH = ?L = 150 m, D = 250 mm, f = 0.0152× bend (K = 0.3)

A pipe 150 m long with an inside diameter of 250 mm (Darcy friction factor f = 0.015) runs from an open reservoir and discharges as a free jet into the air. The minor losses are a square-edged entrance (K = 0.5), 2 bends (K = 0.3 each) and a valve (K = 0.2). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 80 L/s?

Q = 80 L/sL = 150 mD = 250 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 0.2
H = m
23.Pumps & pump powerMedium
PQ = 20 L/sH = 70 m

A pump delivers 20 L/s of water (ρ = 1000 kg/m³) against a head of 70 m. The pump efficiency is 82% and the electric motor driving it has an efficiency of 90%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 20 L/sH = 70 mηpump = 82%ηmotor = 90%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 100 L/sΔz = 10 mL = 600 m, D = 250 mm, f = 0.018, ΣK = 6

A pump moves 100 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 10 m higher. The pipe is 600 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 100 L/sΔz = 10 mL = 600 mD = 250 mmf = 0.018ΣK = 6
H = m

3Solutions

1.Mass balance

Answer: ṁ2 = 66.67 kg/h

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

Balances

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

Solve for ṁ2

ṁ2 = ṁ1(x1 − x3)/(x3 − x2) = 200·(45 − 35)/(35 − 5) = 66.67 kg/h

Answer

ṁ2 = 66.67 kg/h
2.Mass balance

Answer: P = 440 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 = 2200·11/55 = 440 kg/h

Answer

P = 440 kg/h
3.Energy balance

Answer: tout = 32.54 °C

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

Heat released by the hot stream

Q = 0.5·2.1·(130 − 100) = 31.5 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 25 + 31.5/(1·4.18) = 32.54 °C

Answer

tout = 32.54 °C
4.Energy balance

Answer: ṁc = 1.489 kg/s

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

Heat released

Qh = 2.5·2.44·(150 − 90) = 366 kW

Heat that reaches the water

Qc = (1 − 0.15)·366 = 311.1 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 311.1/(4.18·50) = 1.489 kg/s

Answer

ṁc = 1.489 kg/s
5.Ideal gas law

Answer: P = 9249 kPa

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

Moles

n = m/M = 260/16.04 = 16.21 mol
T = 70 + 273.15 = 343.1 K

Pressure

P = nRT/V = 16.21·8.314·343.1/0.005 = 9249 kPa

Answer

P = 9249 kPa
6.Ideal gas law

Answer: ρ = 4.136 kg/m³

Ideal gas density: ρ = PM/(RT).

Rearrange the gas law

PV = (m/M)RT → ρ = m/V = PM/(RT)
T = 100 + 273.15 = 373.1 K

Density

ρ = 800·16.04/(8.314·373.1) = 4.136 kg/m³

Answer

ρ = 4.136 kg/m³
7.Stoichiometry

Answer: m = 36.47 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(N2) = 30/28.02 = 1.071 mol
n(H2) = 20/2.016 = 9.921 mol

Limiting reactant

1.071/1 = 1.071, 9.921/3 = 3.307 → N2

Mass of product

n(NH3) = 1.071·2 = 2.141 mol
m = 2.141·17.03 = 36.47 g

Answer

m = 36.47 g
8.Stoichiometry

Answer: Y = 82 %

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) = 30/2.016 = 14.88 mol
m = 14.88·2/2·18.02 = 268.2 g

Percent yield

Y = 219.9/268.2·100 = 82%

Answer

Y = 82%
9.Chemical equilibrium

Answer: [H2] = 0.02139 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

54 = (2x)²/(0.1 − x)²

Take the square root

7.348 = 2x/(0.1 − x) → x = 0.1·7.348/(2 + 7.348) = 0.07861 mol/L

Equilibrium concentration

[H₂] = 0.1 − x = 0.02139 mol/L

Answer

[H2] = 0.02139 mol/L
10.Chemical equilibrium

Answer: [Cl2] = 0.16 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

0.04 = x²/(0.8 − x) → x² + 0.04·x − 0.032 = 0

Solve the quadratic

x = (−0.04 + √(0.04² + 4·0.032))/2 = 0.16 mol/L

Equilibrium concentration

[Cl₂] = x = 0.16 mol/L

Answer

[Cl2] = 0.16 mol/L
11.Calorimetry & enthalpy

Answer: Tf = 35.54 °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

250·0.385·(90 − Tf) = 100·4.18·(Tf − 23)

Solve for the final temperature

Tf = (96.25·90 + 418·23)/(96.25 + 418) = 35.54 °C

Answer

Tf = 35.54 °C
12.Calorimetry & enthalpy

Answer: q = 1007 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 = 20/44.1 = 0.4535 mol
q = n·|ΔH°/1| = 0.4535·2220 = 1007 kJ

Answer

q = 1007 kJ
13.Reaction kinetics

Answer: k = 0.21 min⁻¹

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).

Integrated first-order law

k = ln(CA0/CA)/t = ln(2/0.7)/5 = 1.05/5 = 0.21 min⁻¹

Answer

k = 0.21 min⁻¹
14.Reaction kinetics

Answer: X = 24.27 %

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).

Rate constant at the new temperature

T1 = 293.1 K, T2 = 313.1 K
k2 = 0.005·e−(50000/8.314)·(1/313.1 − 1/293.1) = 0.01854 min⁻¹

Conversion

X = 1 − e−0.01854·15 = 1 − 0.7573 = 24.27 %

Answer

X = 24.27 %
15.Reactor sizing (CSTR & PFR)

Answer: V = 191.9 L

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 = ln(1/(1 − 0.9))/0.3 = 2.303/0.3 = 7.675 min

Volume

V = Q·τ = 25·7.675 = 191.9 L

Answer

V = 191.9 L
16.Reactor sizing (CSTR & PFR)

Answer: X = 45.12 %

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 = 500/100 = 5 min, kτ = 0.12·5 = 0.6

Conversion

X = 1 − e−kτ = 1 − e−0.6 = 45.12%

Answer

X = 45.12%
17.Heat exchangers (LMTD)

Answer: A = 36.11 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.

Heat duty from the water side

Q̇ = 4·4.18·(125 − 10) = 1923 kW

End temperature differences

ΔT₁ = 140 − 10 = 130 K
ΔT₂ = 140 − 125 = 15 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (130 − 15)/ln(130/15) = 53.25 K

Area

A = Q̇/(U·ΔTlm) = 1.923 × 10⁶/(1000·53.25) = 36.11 m²

Answer

A = 36.11 m²
18.Heat exchangers (LMTD)

Answer: L = 109.9 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 = 0.8·2.1·(125 − 55) = 117.6 kW
Tc,out = 20 + 117.6/(1·4.18) = 48.13 °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 = 125 − 48.13 = 76.87 K
ΔT₂ = Th,out − Tc,in = 55 − 20 = 35 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (76.87 − 35)/ln(76.87/35) = 53.22 K

Area and length

A = 117600/(200·53.22) = 11.05 m²
L = A/(πD) = 11.05/(π·0.032) = 109.9 m

Answer

L = 109.9 m
19.Heat conduction

Answer: Ti = 19.34 °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)/(0.17·8) = 0.1838 K/W
R2 = L2/(k2A) = (150/1000)/(0.04·8) = 0.4688 K/W

Heat flow

Q̇ = (T1 − T3)/(R1 + R2) = 13/0.6526 = 19.92 W

Interface temperature

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

Ti = T1 − Q̇·R1 = 23 − 19.92·0.1838 = 19.34 °C

Answer

Ti = 19.34 °C
20.Heat conduction

Answer: Q̇ = 104 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/(10·6) = 0.01667 K/W
R1 = L1/(k1A) = (50/1000)/(0.035·6) = 0.2381 K/W
R2 = L2/(k2A) = (75/1000)/(0.72·6) = 0.01736 K/W
Ro = 1/(hoA) = 1/(25·6) = 0.006667 K/W
ΣR = 0.2788 K/W

Heat loss

Q̇ = (22 − (-7))/0.2788 = 104 W

Answer

Q̇ = 104 W
21.Pipe friction & head loss

Answer: Δp = 32.67 kPa

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.

Head loss

hf = f·(L/D)·V²/(2g) = 0.025·(100/0.3)·2.8²/(2·9.81) = 3.33 m

Pressure drop

The pipe is horizontal and the velocity does not change, so the energy equation reduces to Δp = ρ·g·hf.

Δp = ρ·g·hf = 1000·9.81·3.33 = 32667 Pa = 32.67 kPa

Answer

Δp = 32.67 kPa
22.Pipe friction & head loss

Answer: H = 1.53 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

V = Q/A = 0.08/0.04909 = 1.63 m/s
V²/(2g) = 0.1354 m

Loss coefficients

f·L/D = 0.015·150/0.25 = 9
ΣK = 0.5 + 2·0.3 + 0.2 = 1.3

Energy equation

The outlet jet still carries its velocity head; it is not a loss but it has to be supplied.

H = (1 + 9 + 1.3)·0.1354 = 1.53 m

Answer

H = 1.53 m
23.Pumps & pump power

Answer: Pel = 18.61 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 = 1000·9.81·0.02·70 = 13.73 kW

Shaft power

Pshaft = 13.73/0.82 = 16.75 kW

Electrical power

Pel = 16.75/0.9 = 18.61 kW

Answer

Pel = 18.61 kW
24.Pumps & pump power

Answer: H = 20.41 m

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 = 0.1/0.04909 = 2.037 m/s
V²/(2g) = 0.2115 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (43.2 + 6)·0.2115 = 10.41 m

Pump head

Both surfaces are open and practically at rest, so pressure and velocity terms drop out.

H = Δz + hL = 10 + 10.41 = 20.41 m

Answer

H = 20.41 m

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