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 1550 kg/h · 35% saltStream 2ṁ₂ = ? · 5% saltProduct15% salt

How much of stream 2 must be added each hour to stream 1 so that the blended product contains 15% salt? Find ṁ2.

ṁ1 = 550 kg/hx1 = 35 %x2 = 5 %x3 = 15 %
ṁ2 = kg/h
2.Mass balanceHard
EvaporatorFeed F4000 kg/h · 17% NaOHProduct PP = ? · 65%Vapour W (pure water)0% NaOH

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

F = 4000 kg/hxF = 17 %xP = 65 %
P = kg/h
3.Energy balanceMedium
hot sidecold sideethanol · 120 °C70 °Cwater · 15 °Ct = ? °C

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

ṁh = 2.5 kg/scp,h = 2.44 kJ/(kg·K)Th: 120 → 70 °Cṁc = 2 kg/scp,c = 4.18 kJ/(kg·K)tin = 15 °C
tout = °C
4.Energy balanceHard
hot sidecold sideethanol · 130 °C60 °Cwater · 15 °C65 °C · ṁ = ?10% lost

Hot ethanol heats water in an exchanger that loses 10% 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: 130 → 60 °Ct: 15 → 65 °Ccp,c = 4.18 kJ/(kg·K)loss = 10 %
ṁc = kg/s
5.Ideal gas lawMedium
160 g of ArP = 500 kPaT = 0 °CV = ?

What volume V does 160 g of Ar occupy at 500 kPa and 0 °C? Treat it as an ideal gas.

m = 160 gM = 39.95 g/molP = 500 kPaT = 0 °CR = 8.314 J/(mol·K)
V = L
6.Ideal gas lawHard
O₂, M = 32 g/molP = 750 kPaT = 120 °Cρ = ?

Find the density ρ of O₂ at 750 kPa and 120 °C, treating it as an ideal gas.

M = 32 g/molP = 750 kPaT = 120 °CR = 8.314 J/(mol·K)
ρ = kg/m³
7.StoichiometryMedium
m(X)n(X)n(MgO)m(MgO)÷ M(X)× 2/ν× M(MgO)

8 g of Mg and 16 g of O2 react according to 2Mg + O2 → 2MgO. What mass m of MgO can form?

M(Mg) = 24.31M(O2) = 32M(MgO) = 40.3 g/mol
m = g
8.StoichiometryHard
m(CH4​)n(CH4​)n(H2​O)m(H2​O)÷ M(CH4​)× 2/1× M(H2​O)

In the reaction CH4 + 2O2 → CO2 + 2H2O, 4 g of CH4 reacts completely (the other reactants are in excess) and 7.64 g of H2O is collected. Find the percent yield Y.

M(CH4) = 16.04 g/molM(H2O) = 18.02 g/molactual: 7.64 g
Y = %
9.Chemical equilibriumMedium
H2​I2​HII0.40.40C−x−x+2xE0.4 − x0.4 − x2x

0.4 mol/L of H₂ and 0.4 mol/L of I₂ are put in a container and react: H₂ + I₂ ⇌ 2HI, with Kc = 25. Find the equilibrium concentration [HI].

[H₂]₀ = [I₂]₀ = 0.4 mol/LKc = 25
[HI] = mol/L
10.Chemical equilibriumHard
PCl5​PCl3​Cl2​I0.100C−x+x+xE0.1 − xxx

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

[PCl₅]₀ = 0.1 mol/LKc = 0.1
[Cl2] = mol/L
11.Calorimetry & enthalpyMedium
Tf​ = ?Zincm = 150 gT = 150 °Cc = 0.388 J/(g·°C)Waterm = 200 gT = 19 °Cc = 4.18 J/(g·°C)

A 150 g block of zinc (c = 0.388 J/(g·°C)) at 150 °C is dropped into 200 g of water (c = 4.18 J/(g·°C)) at 19 °C in an insulated cup. Find the final temperature Tf.

mmetal = 150 gcmetal = 0.388 J/(g·°C)Tmetal = 150 °Cmwater = 200 gTwater = 19 °Ccwater = 4.18 J/(g·°C)
Tf = °C
12.Calorimetry & enthalpyHard
H10 g C4​H10​2C4​H10​ + 13O₂reactants8CO₂ + 10H₂O(l)productsq = ?

Use the standard enthalpies of formation to find the heat q released when 10 g of C4H10 (M = 58.12 g/mol) burns completely: 2C4H10 + 13O₂ → 8CO₂ + 10H₂O(l). Give q as a positive number.

ΔH°f(C4H10) = −125.6 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 second-order reaction (−rA = k·CA²) in a batch reactor has k = 0.25 L/(mol·min) and starts at 1 mol/L. How long does it take to reach 50% conversion? Find t.

k = 0.25 L/(mol·min)CA0 = 1 mol/LX = 50 %
t = min
14.Reaction kineticsHard
1/Tln kT = 25 °Cln 0.05ln A = ?Ea​ = 50 kJ/mol

A first-order reaction has a rate constant of 0.05 s⁻¹ at 25 °C and an activation energy of 50 kJ/mol. Find the pre-exponential factor A in the Arrhenius equation.

k = 0.05 s⁻¹T = 25 °CEa = 50 kJ/molR = 8.314 J/(mol·K)
A = s⁻¹
15.Reactor sizing (CSTR & PFR)Medium
Q = 40 L/minCA0​ = 2 mol/LCA​ = ?V = 200 L, k = 0.25 min⁻¹

A liquid-phase first-order reaction A → B (k = 0.25 min⁻¹) runs in a 200 L plug-flow reactor (PFR). The feed enters at 40 L/min with CA0 = 2 mol/L. The density is constant and the reactor is at steady state. Find the outlet concentration CA.

V = 200 LQ = 40 L/mink = 0.25 min⁻¹CA0 = 2 mol/L
CA = mol/L
16.Reactor sizing (CSTR & PFR)Hard
V = 150 LV = 150 LQ = 40 L/minX = ?

A first-order liquid-phase reaction (k = 0.3 min⁻¹) runs in two equal CSTRs in series, each of 150 L. The feed rate is 40 L/min, the density is constant and the reactors are at steady state. Find the overall conversion X in percent.

V = 150 L (×2)Q = 40 L/mink = 0.3 min⁻¹
X = %
17.Heat exchangers (LMTD)Medium
lengthT175 °C65 °C80 °C20 °CΔT₁ΔT₂counter-flow

A shell-and-tube heat exchanger (one shell pass, two tube passes) must transfer 180 kW. The hot fluid cools from 175 to 65 °C and the cold fluid heats from 20 to 80 °C. The LMTD correction factor for this arrangement is F = 0.85, and U = 300 W/(m²·K). Find the heat transfer area A needed.

Q̇ = 180 kWF = 0.85U = 300 W/(m²·K)Th: 175 → 65 °CTc: 20 → 80 °C
A = m²
18.Heat exchangers (LMTD)Hard
lengthT125 °C45 °C22.34 °C15 °CΔT₁ΔT₂counter-flow

Hot oil (0.5 kg/s, cp = 2.3 kJ/(kg·K)) cools from 125 to 45 °C in a counter-flow exchanger. It heats 3 kg/s of water (cp = 4.18 kJ/(kg·K)) that enters at 15 °C. With U = 800 W/(m²·K), find the heat transfer area A needed.

ṁh = 0.5 kg/scp,h = 2.3 kJ/(kg·K)Th: 125 → 45 °Cṁc = 3 kg/scp,c = 4.18 kJ/(kg·K)Tc,in = 15 °CU = 800 W/(m²·K)
A = m²
19.Heat conductionMedium
Expanded polystyrene, k = 0.035100 mmMineral wool, k = 0.04150 mm21 °C-9 °CTi​ = ?Q̇

A wall is made of 100 mm of expanded polystyrene and 150 mm of mineral wool, with an area of 20 m². The outer faces are at 21 °C and -9 °C. Find the temperature Ti at the interface between the two layers.

L1 = 100 mm, k1 = 0.035 W/(m·K)L2 = 150 mm, k2 = 0.04 W/(m·K)A = 20 m²T1 = 21 °CT3 = -9 °C
Ti = °C
20.Heat conductionHard
Gypsum board, k = 0.17200 mmBrick, k = 0.7250 mmroom 20 °Coutside -8 °CQ̇

A wall of 200 mm gypsum board and 50 mm brick separates a room at 20 °C from outside air at -8 °C. The convection coefficients are 7.7 W/(m²·K) inside and 30 W/(m²·K) outside, and the wall area is 4 m². Find the overall heat transfer coefficient U of the wall.

L1 = 200 mm, k1 = 0.17 W/(m·K)L2 = 50 mm, k2 = 0.72 W/(m·K)A = 4 m²hi = 7.7 W/(m²·K)ho = 30 W/(m²·K)Troom = 20 °CTout = -8 °C
U = W/(m²·K)
21.Pipe friction & head lossMedium
V = 2.3 m/sD = 300 mmL = 150 mf = 0.03

Water (ρ = 1000 kg/m³) flows at 2.3 m/s through a horizontal pipe, 150 m long, with an inside diameter of 300 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 2.3 m/sL = 150 mD = 300 mmf = 0.03ρ = 1000 kg/m³
Δp = kPa
22.Pipe friction & head lossHard
K = 2free outletH = ?L = 400 m, D = 300 mm, f = 0.0183× bend (K = 0.3)

A pipe 400 m long with an inside diameter of 300 mm (Darcy friction factor f = 0.018) 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), 3 bends (K = 0.3 each) and a valve (K = 2). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 200 L/s?

Q = 200 L/sL = 400 mD = 300 mmf = 0.018Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 2
H = m
23.Pumps & pump powerMedium
PQ = 50 L/sH = 60 m

A pump delivers 50 L/s of water (ρ = 1000 kg/m³) against a head of 60 m. The pump efficiency is 65% 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 = 50 L/sH = 60 mηpump = 65%ηmotor = 90%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
350 kPa (gauge)PQ = 60 L/sΔz = 9 mL = 400 m, D = 200 mm, f = 0.022, ΣK = 6

A pump moves 60 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 400 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.022; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². The upper tank is closed and the air above its water is at a gauge pressure of 350 kPa. Find the head H the pump must add.

Q = 60 L/sΔz = 9 mL = 400 mD = 200 mmf = 0.022ΣK = 6ptank = 350 kPa
H = m

3Solutions

1.Mass balance

Answer: ṁ2 = 1100 kg/h

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

Balances

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

Solve for ṁ2

ṁ2 = ṁ1(x1 − x3)/(x3 − x2) = 550·(35 − 15)/(15 − 5) = 1100 kg/h

Answer

ṁ2 = 1100 kg/h
2.Mass balance

Answer: P = 1046 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 = 4000·17/65 = 1046 kg/h

Answer

P = 1046 kg/h
3.Energy balance

Answer: tout = 51.48 °C

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

Heat released by the hot stream

Q = 2.5·2.44·(120 − 70) = 305 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 15 + 305/(2·4.18) = 51.48 °C

Answer

tout = 51.48 °C
4.Energy balance

Answer: ṁc = 1.839 kg/s

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

Heat released

Qh = 2.5·2.44·(130 − 60) = 427 kW

Heat that reaches the water

Qc = (1 − 0.1)·427 = 384.3 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 384.3/(4.18·50) = 1.839 kg/s

Answer

ṁc = 1.839 kg/s
5.Ideal gas law

Answer: V = 18.19 L

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

Moles

n = 160/39.95 = 4.005 mol
T = 0 + 273.15 = 273.1 K

Volume

V = nRT/P = 4.005·8.314·273.1/500 = 18.19 L

Answer

V = 18.19 L
6.Ideal gas law

Answer: ρ = 7.342 kg/m³

Ideal gas density: ρ = PM/(RT).

Rearrange the gas law

PV = (m/M)RT → ρ = m/V = PM/(RT)
T = 120 + 273.15 = 393.1 K

Density

ρ = 750·32/(8.314·393.1) = 7.342 kg/m³

Answer

ρ = 7.342 kg/m³
7.Stoichiometry

Answer: m = 13.26 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(Mg) = 8/24.31 = 0.3291 mol
n(O2) = 16/32 = 0.5 mol

Limiting reactant

0.3291/2 = 0.1645, 0.5/1 = 0.5 → Mg

Mass of product

n(MgO) = 0.1645·2 = 0.3291 mol
m = 0.3291·40.3 = 13.26 g

Answer

m = 13.26 g
8.Stoichiometry

Answer: Y = 85.01 %

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(CH4) = 4/16.04 = 0.2494 mol
m = 0.2494·2/1·18.02 = 8.988 g

Percent yield

Y = 7.64/8.988·100 = 85.01%

Answer

Y = 85.01%
9.Chemical equilibrium

Answer: [HI] = 0.5714 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

25 = (2x)²/(0.4 − x)²

Take the square root

5 = 2x/(0.4 − x) → x = 0.4·5/(2 + 5) = 0.2857 mol/L

Equilibrium concentration

[HI] = 2x = 0.5714 mol/L

Answer

[HI] = 0.5714 mol/L
10.Chemical equilibrium

Answer: [Cl2] = 0.0618 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

0.1 = x²/(0.1 − x) → x² + 0.1·x − 0.01 = 0

Solve the quadratic

x = (−0.1 + √(0.1² + 4·0.01))/2 = 0.0618 mol/L

Equilibrium concentration

[Cl₂] = x = 0.0618 mol/L

Answer

[Cl2] = 0.0618 mol/L
11.Calorimetry & enthalpy

Answer: Tf = 27.53 °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

150·0.388·(150 − Tf) = 200·4.18·(Tf − 19)

Solve for the final temperature

Tf = (58.2·150 + 836·19)/(58.2 + 836) = 27.53 °C

Answer

Tf = 27.53 °C
12.Calorimetry & enthalpy

Answer: q = 495.1 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° = [8·(−393.5) + 10·(−285.8)] − [2·(−125.6) + 13·0] = −5755 kJ

Heat for the given mass

n = 10/58.12 = 0.1721 mol
q = n·|ΔH°/2| = 0.1721·2877 = 495.1 kJ

Answer

q = 495.1 kJ
13.Reaction kinetics

Answer: t = 4 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).

Concentration at the end

CA = 1·(1 − 0.5) = 0.5 mol/L

Integrated second-order law

t = (1/CA − 1/CA0)/k = (2 − 1)/0.25 = 4 min

Answer

t = 4 min
14.Reaction kinetics

Answer: A = 2.878 × 10⁷ s⁻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 temperature

T = 25 + 273.15 = 298.1 K

Solve Arrhenius for A

Ea/(RT) = 50000/(8.314·298.1) = 20.17
A = k·e20.17 = 0.05·5.756 × 10⁸ = 2.878 × 10⁷ s⁻¹

Answer

A = 2.878 × 10⁷ s⁻¹
15.Reactor sizing (CSTR & PFR)

Answer: CA = 0.573 mol/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 = V/Q = 200/40 = 5 min

Outlet concentration

CA = 2·e−0.25·5 = 0.573 mol/L

Answer

CA = 0.573 mol/L

Conversion: X = 71.35%.

16.Reactor sizing (CSTR & PFR)

Answer: X = 77.85 %

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 = 150/40 = 3.75 min, kτ = 0.3·3.75 = 1.125

Conversion

C1/CA0 = 1/(1 + kτ) = 1/(1 + 1.125) = 0.4706
C2/CA0 = 1/(1 + kτ)² = 0.2215
X = 1 − 0.2215 = 77.85%

Answer

X = 77.85%
17.Heat exchangers (LMTD)

Answer: A = 10.55 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 = 175 − 80 = 95 K
ΔT₂ = Th,out − Tc,in = 65 − 20 = 45 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (95 − 45)/ln(95/45) = 66.92 K

Area

A = Q̇/(U·F·ΔTlm,cf) = 180000/(300·0.85·66.92) = 10.55 m²

Answer

A = 10.55 m²
18.Heat exchangers (LMTD)

Answer: A = 1.947 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 and water outlet temperature

Q̇ = ṁhcp,h(Th,in − Th,out) = 0.5·2.3·80 = 92 kW
Tc,out = 15 + 92/(3·4.18) = 22.34 °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 − 22.34 = 102.7 K
ΔT₂ = Th,out − Tc,in = 45 − 15 = 30 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (102.7 − 30)/ln(102.7/30) = 59.06 K

Area

A = Q̇/(U·ΔTlm) = 92000/(800·59.06) = 1.947 m²

Answer

A = 1.947 m²
19.Heat conduction

Answer: Ti = 8.027 °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) = (100/1000)/(0.035·20) = 0.1429 K/W
R2 = L2/(k2A) = (150/1000)/(0.04·20) = 0.1875 K/W

Heat flow

Q̇ = (T1 − T3)/(R1 + R2) = 30/0.3304 = 90.81 W

Interface temperature

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

Ti = T1 − Q̇·R1 = 21 − 90.81·0.1429 = 8.027 °C

Answer

Ti = 8.027 °C
20.Heat conduction

Answer: U = 0.7097 W/(m²·K)

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/(7.7·4) = 0.03247 K/W
R1 = L1/(k1A) = (200/1000)/(0.17·4) = 0.2941 K/W
R2 = L2/(k2A) = (50/1000)/(0.72·4) = 0.01736 K/W
Ro = 1/(hoA) = 1/(30·4) = 0.008333 K/W
ΣR = 0.3523 K/W

Overall coefficient

U = 1/(A·ΣR) = 1/(4·0.3523) = 0.7097 W/(m²·K)

Answer

U = 0.7097 W/(m²·K)
21.Pipe friction & head loss

Answer: Δp = 39.67 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) = 0.03·(150/0.3)·2.3²/(2·9.81) = 4.044 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 = 1000·9.81·4.044 = 39675 Pa = 39.67 kPa

Answer

Δp = 39.67 kPa
22.Pipe friction & head loss

Answer: H = 11.59 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 = 0.2/0.07069 = 2.829 m/s
V²/(2g) = 0.408 m

Loss coefficients

f·L/D = 0.018·400/0.3 = 24
ΣK = 0.5 + 3·0.3 + 2 = 3.4

Energy equation

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

H = (1 + 24 + 3.4)·0.408 = 11.59 m

Answer

H = 11.59 m
23.Pumps & pump power

Answer: Pel = 50.31 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 = 1000·9.81·0.05·60 = 29.43 kW

Shaft power

Pshaft = 29.43/0.65 = 45.28 kW

Electrical power

Pel = 45.28/0.9 = 50.31 kW

Answer

Pel = 50.31 kW
24.Pumps & pump power

Answer: H = 53.97 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 = 0.06/0.03142 = 1.91 m/s
V²/(2g) = 0.1859 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (44 + 6)·0.1859 = 9.296 m

Pressure head

p/(ρ·g) = 350000/(1000·9.81) = 35.68 m

Pump head

Both surfaces are practically at rest, so there is no velocity head term.

H = Δz + p/(ρ·g) + hL = 9 + 35.68 + 9.296 = 53.97 m

Answer

H = 53.97 m

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