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 1450 kg/h · 45% sugarStream 2ṁ₂ = ? · 20% sugarProduct40% sugar

How much of stream 2 must be added each hour to stream 1 so that the blended product contains 40% sugar? Find ṁ2.

ṁ1 = 450 kg/hx1 = 45 %x2 = 20 %x3 = 40 %
ṁ2 = kg/h
2.Mass balanceHard
EvaporatorFeed F3800 kg/h · 12% saltProduct P55% saltVapour W (pure water)W = ? kg/h

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

F = 3800 kg/hxF = 12 %xP = 55 %
W = kg/h
3.Energy balanceMedium
hot sidecold sideglycol mix · 170 °C90 °Cwater · 25 °Ct = ? °C

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

ṁh = 1 kg/scp,h = 3.6 kJ/(kg·K)Th: 170 → 90 °Cṁc = 2 kg/scp,c = 4.18 kJ/(kg·K)tin = 25 °C
tout = °C
4.Energy balanceHard
hot sidecold sidelight oil · 170 °C100 °Cwater · 15 °C90 °C · ṁ = ?5% lost

Hot light oil 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 = 3 kg/scp,h = 2.1 kJ/(kg·K)Th: 170 → 100 °Ct: 15 → 90 °Ccp,c = 4.18 kJ/(kg·K)loss = 5 %
ṁc = kg/s
5.Ideal gas lawMedium
300 g of CO₂V = 30 LT = 20 °CP = ?

A tank of 30 L contains 300 g of CO₂ at 20 °C. Treat it as an ideal gas and find the pressure P.

m = 300 gM = 44.01 g/molV = 30 LT = 20 °CR = 8.314 J/(mol·K)
P = kPa
6.Ideal gas lawHard
O₂, M = 32 g/molP = 100 kPaT = 170 °Cρ = ?

Find the density ρ of O₂ at 100 kPa and 170 °C, treating it as an ideal gas.

M = 32 g/molP = 100 kPaT = 170 °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)

10 g of C3H8 and 24 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(CaCO3​)n(CaCO3​)n(CaO)m(CaO)÷ M(CaCO3​)× 1/1× M(CaO)

In the reaction CaCO3 → CaO + CO2, 10 g of CaCO3 reacts completely (the other reactants are in excess) and 5.1 g of CaO is collected. Find the percent yield Y.

M(CaCO3) = 100.09 g/molM(CaO) = 56.08 g/molactual: 5.1 g
Y = %
9.Chemical equilibriumMedium
H2​I2​HII0.50.50C−x−x+2xE0.5 − x0.5 − x2x

0.5 mol/L of H₂ and 0.5 mol/L of I₂ are put in a container and react: H₂ + I₂ ⇌ 2HI, with Kc = 4. Find the equilibrium concentration [H2].

[H₂]₀ = [I₂]₀ = 0.5 mol/LKc = 4
[H2] = mol/L
10.Chemical equilibriumHard
PCl5​PCl3​Cl2​I0.400C−x+x+xE0.4 − xxx

PCl₅ decomposes: PCl₅ ⇌ PCl₃ + Cl₂, with Kc = 0.01 at the reaction temperature. A container starts with 0.4 mol/L of PCl₅ only. Find the equilibrium concentration [Cl2].

[PCl₅]₀ = 0.4 mol/LKc = 0.01
[Cl2] = mol/L
11.Calorimetry & enthalpyMedium
Tf​ = ?Aluminiumm = 200 gT = 110 °Cc = 0.897 J/(g·°C)Waterm = 400 gT = 24 °Cc = 4.18 J/(g·°C)

A 200 g block of aluminium (c = 0.897 J/(g·°C)) at 110 °C is dropped into 400 g of water (c = 4.18 J/(g·°C)) at 24 °C in an insulated cup. Find the final temperature Tf.

mmetal = 200 gcmetal = 0.897 J/(g·°C)Tmetal = 110 °Cmwater = 400 gTwater = 24 °Ccwater = 4.18 J/(g·°C)
Tf = °C
12.Calorimetry & enthalpyHard
HC2​H5​OH + 3O₂reactants2CO₂ + 3H₂O(l)productsΔH° = ?

Use the standard enthalpies of formation to find ΔH° for the reaction C2H5OH + 3O₂ → 2CO₂ + 3H₂O(l).

ΔH°f(C2H5OH) = −277.7 kJ/molΔH°f(CO₂) = −393.5 kJ/molΔH°f(H₂O, l) = −285.8 kJ/molΔH°f(O₂) = 0
ΔH° = kJ
13.Reaction kineticsMedium
t (min)X (%)t = ?80%

A second-order reaction (−rA = k·CA²) in a batch reactor has k = 0.05 L/(mol·min) and starts at 0.5 mol/L. How long does it take to reach 80% conversion? Find t.

k = 0.05 L/(mol·min)CA0 = 0.5 mol/LX = 80 %
t = min
14.Reaction kineticsHard
1/Tln kT = 50 °Cln 0.002ln A = ?Ea​ = 70 kJ/mol

A first-order reaction has a rate constant of 0.002 s⁻¹ at 50 °C and an activation energy of 70 kJ/mol. Find the pre-exponential factor A in the Arrhenius equation.

k = 0.002 s⁻¹T = 50 °CEa = 70 kJ/molR = 8.314 J/(mol·K)
A = s⁻¹
15.Reactor sizing (CSTR & PFR)Medium
Q = 25 L/minX = 85%V = ?, k = 0.5 min⁻¹

A first-order liquid-phase reaction A → B with k = 0.5 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 85% conversion of A.

Q = 25 L/mink = 0.5 min⁻¹X = 85%
V = L
16.Reactor sizing (CSTR & PFR)Hard
V = 50 LQ = 40 L/minX = ?

A first-order liquid-phase reaction (k = 0.25 min⁻¹) runs in a 50 L CSTR fed at 40 L/min. The density is constant and the reactor is at steady state. Find the conversion X in percent.

V = 50 LQ = 40 L/mink = 0.25 min⁻¹
X = %
17.Heat exchangers (LMTD)Medium
lengthT125 °C110 °C15 °C65 °CΔT₁ΔT₂parallel flow

A parallel-flow heat exchanger transfers 200 kW. The hot fluid cools from 125 to 110 °C and the cold fluid heats from 15 to 65 °C. The overall heat transfer coefficient is 1000 W/(m²·K). Find the heat transfer area A needed.

Q̇ = 200 kWU = 1000 W/(m²·K)Th: 125 → 110 °CTc: 15 → 65 °C
A = m²
18.Heat exchangers (LMTD)Hard
lengthT120 °C10 °C?ΔT₁ΔT₂condensing steam

Steam condenses at a constant 120 °C on the outside of the tubes of a condenser with a heat transfer area of 1.5 m² and U = 3000 W/(m²·K). Cooling water (2 kg/s, cp = 4.18 kJ/(kg·K)) enters the tubes at 10 °C. Find the water outlet temperature Tc,out.

Ts = 120 °CA = 1.5 m²U = 3000 W/(m²·K)ṁ = 2 kg/scp = 4.18 kJ/(kg·K)Tc,in = 10 °C
Tc,out = °C
19.Heat conductionMedium
Gypsum board, k = 0.17250 mmWood, k = 0.1775 mm18 °C2 °CTi​ = ?Q̇

A wall is made of 250 mm of gypsum board and 75 mm of wood, with an area of 20 m². The outer faces are at 18 °C and 2 °C. Find the temperature Ti at the interface between the two layers.

L1 = 250 mm, k1 = 0.17 W/(m·K)L2 = 75 mm, k2 = 0.17 W/(m·K)A = 20 m²T1 = 18 °CT3 = 2 °C
Ti = °C
20.Heat conductionHard
Concrete, k = 1.4200 mmBrick, k = 0.72100 mmroom 22 °Coutside -6 °CQ̇

A wall of 200 mm concrete and 100 mm brick separates a room at 22 °C from outside air at -6 °C. The convection coefficients are 6 W/(m²·K) inside and 30 W/(m²·K) outside, and the wall area is 12 m². Find the overall heat transfer coefficient U of the wall.

L1 = 200 mm, k1 = 1.4 W/(m·K)L2 = 100 mm, k2 = 0.72 W/(m·K)A = 12 m²hi = 6 W/(m²·K)ho = 30 W/(m²·K)Troom = 22 °CTout = -6 °C
U = W/(m²·K)
21.Pipe friction & head lossMedium
V = 1.1 m/sD = 200 mmL = 400 mf = 0.018

Water (ρ = 1000 kg/m³) flows at 1.1 m/s through a horizontal pipe, 400 m long, with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.018 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 1.1 m/sL = 400 mD = 200 mmf = 0.018ρ = 1000 kg/m³
Δp = kPa
22.Pipe friction & head lossHard
K = 10free outletH = ?L = 100 m, D = 150 mm, f = 0.0184× bend (K = 0.3)

A pipe 100 m long with an inside diameter of 150 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), 4 bends (K = 0.3 each) and a valve (K = 10). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 20 L/s?

Q = 20 L/sL = 100 mD = 150 mmf = 0.018Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 10
H = m
23.Pumps & pump powerMedium
PQ = 30 L/sH = 78 m

A pump with an efficiency of 85% delivers 30 L/s of water (ρ = 1000 kg/m³) against a head of 78 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 30 L/sH = 78 mη = 85%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 60 L/sΔz = 7 mL = 150 m, D = 200 mm, f = 0.02, ΣK = 3

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 7 m higher. The pipe is 150 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.02; the minor-loss coefficients add up to ΣK = 3 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 72%. Find the shaft power Pshaft in kW.

Q = 60 L/sΔz = 7 mL = 150 mD = 200 mmf = 0.02ΣK = 3η = 72%
Pshaft = kW

3Solutions

1.Mass balance

Answer: ṁ2 = 112.5 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) = 450·(45 − 40)/(40 − 20) = 112.5 kg/h

Answer

ṁ2 = 112.5 kg/h
2.Mass balance

Answer: W = 2971 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 = 3800·12/55 = 829.1 kg/h

Total balance

W = F − P = 3800 − 829.1 = 2971 kg/h

Answer

W = 2971 kg/h
3.Energy balance

Answer: tout = 59.45 °C

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

Heat released by the hot stream

Q = 1·3.6·(170 − 90) = 288 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 25 + 288/(2·4.18) = 59.45 °C

Answer

tout = 59.45 °C
4.Energy balance

Answer: ṁc = 1.336 kg/s

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

Heat released

Qh = 3·2.1·(170 − 100) = 441 kW

Heat that reaches the water

Qc = (1 − 0.05)·441 = 419 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 419/(4.18·75) = 1.336 kg/s

Answer

ṁc = 1.336 kg/s
5.Ideal gas law

Answer: P = 553.8 kPa

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

Moles

n = m/M = 300/44.01 = 6.817 mol
T = 20 + 273.15 = 293.1 K

Pressure

P = nRT/V = 6.817·8.314·293.1/0.03 = 553.8 kPa

Answer

P = 553.8 kPa
6.Ideal gas law

Answer: ρ = 0.8685 kg/m³

Ideal gas density: ρ = PM/(RT).

Rearrange the gas law

PV = (m/M)RT → ρ = m/V = PM/(RT)
T = 170 + 273.15 = 443.1 K

Density

ρ = 100·32/(8.314·443.1) = 0.8685 kg/m³

Answer

ρ = 0.8685 kg/m³
7.Stoichiometry

Answer: m = 10.81 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) = 10/44.1 = 0.2268 mol
n(O2) = 24/32 = 0.75 mol

Limiting reactant

0.2268/1 = 0.2268, 0.75/5 = 0.15 → O2

Mass of product

n(H2O) = 0.15·4 = 0.6 mol
m = 0.6·18.02 = 10.81 g

Answer

m = 10.81 g
8.Stoichiometry

Answer: Y = 91.02 %

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(CaCO3) = 10/100.09 = 0.09991 mol
m = 0.09991·1/1·56.08 = 5.603 g

Percent yield

Y = 5.1/5.603·100 = 91.02%

Answer

Y = 91.02%
9.Chemical equilibrium

Answer: [H2] = 0.25 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

4 = (2x)²/(0.5 − x)²

Take the square root

2 = 2x/(0.5 − x) → x = 0.5·2/(2 + 2) = 0.25 mol/L

Equilibrium concentration

[H₂] = 0.5 − x = 0.25 mol/L

Answer

[H2] = 0.25 mol/L
10.Chemical equilibrium

Answer: [Cl2] = 0.05844 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

0.01 = x²/(0.4 − x) → x² + 0.01·x − 0.004 = 0

Solve the quadratic

x = (−0.01 + √(0.01² + 4·0.004))/2 = 0.05844 mol/L

Equilibrium concentration

[Cl₂] = x = 0.05844 mol/L

Answer

[Cl2] = 0.05844 mol/L
11.Calorimetry & enthalpy

Answer: Tf = 32.33 °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

200·0.897·(110 − Tf) = 400·4.18·(Tf − 24)

Solve for the final temperature

Tf = (179.4·110 + 1672·24)/(179.4 + 1672) = 32.33 °C

Answer

Tf = 32.33 °C
12.Calorimetry & enthalpy

Answer: ΔH° = −1367 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° = [2·(−393.5) + 3·(−285.8)] − [1·(−277.7) + 3·0] = −1367 kJ

Answer

ΔH° = −1367 kJ

Negative: the reaction gives off heat (exothermic).

13.Reaction kinetics

Answer: t = 160 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 = 0.5·(1 − 0.8) = 0.1 mol/L

Integrated second-order law

t = (1/CA − 1/CA0)/k = (10 − 2)/0.05 = 160 min

Answer

t = 160 min
14.Reaction kinetics

Answer: A = 4.134 × 10⁸ 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 = 50 + 273.15 = 323.1 K

Solve Arrhenius for A

Ea/(RT) = 70000/(8.314·323.1) = 26.05
A = k·e26.05 = 0.002·2.067 × 10¹¹ = 4.134 × 10⁸ s⁻¹

Answer

A = 4.134 × 10⁸ s⁻¹
15.Reactor sizing (CSTR & PFR)

Answer: V = 94.86 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 − 0.85))/0.5 = 1.897/0.5 = 3.794 min

Volume

V = Q·τ = 25·3.794 = 94.86 L

Answer

V = 94.86 L
16.Reactor sizing (CSTR & PFR)

Answer: X = 23.81 %

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 = 50/40 = 1.25 min, kτ = 0.25·1.25 = 0.3125

Conversion

X = kτ/(1 + kτ) = 0.3125/(1 + 0.3125) = 23.81%

Answer

X = 23.81%
17.Heat exchangers (LMTD)

Answer: A = 2.75 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

In parallel flow both inlets are at the same end, and both outlets at the other.

ΔT₁ = Th,in − Tc,in = 125 − 15 = 110 K
ΔT₂ = Th,out − Tc,out = 110 − 65 = 45 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (110 − 45)/ln(110/45) = 72.72 K

Area

A = Q̇/(U·ΔTlm) = 200000/(1000·72.72) = 2.75 m²

Answer

A = 2.75 m²
18.Heat exchangers (LMTD)

Answer: Tc,out = 55.79 °C

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.

Combine the energy balance and the rate equation

With ΔT₁ = Ts − Tc,in and ΔT₂ = Ts − Tc,out, the difference ΔT₁ − ΔT₂ equals the water temperature rise, so the rise cancels.

ṁcp(ΔT₁ − ΔT₂) = U·A·(ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂)
ln(ΔT₁/ΔT₂) = U·A/(ṁcp) = 3000·1.5/(2·4180) = 0.5383

Outlet temperature

ΔT₂ = ΔT₁·e−0.5383 = 110·0.5838 = 64.21 K
Tc,out = 120 − 64.21 = 55.79 °C

Answer

Tc,out = 55.79 °C

Heat transferred: Q̇ = 382.8 kW.

19.Heat conduction

Answer: Ti = 5.692 °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)/(0.17·20) = 0.07353 K/W
R2 = L2/(k2A) = (75/1000)/(0.17·20) = 0.02206 K/W

Heat flow

Q̇ = (T1 − T3)/(R1 + R2) = 16/0.09559 = 167.4 W

Interface temperature

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

Ti = T1 − Q̇·R1 = 18 − 167.4·0.07353 = 5.692 °C

Answer

Ti = 5.692 °C
20.Heat conduction

Answer: U = 2.076 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/(6·12) = 0.01389 K/W
R1 = L1/(k1A) = (200/1000)/(1.4·12) = 0.0119 K/W
R2 = L2/(k2A) = (100/1000)/(0.72·12) = 0.01157 K/W
Ro = 1/(hoA) = 1/(30·12) = 0.002778 K/W
ΣR = 0.04015 K/W

Overall coefficient

U = 1/(A·ΣR) = 1/(12·0.04015) = 2.076 W/(m²·K)

Answer

U = 2.076 W/(m²·K)
21.Pipe friction & head loss

Answer: Δp = 21.78 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) = 0.018·(400/0.2)·1.1²/(2·9.81) = 2.22 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 = 1000·9.81·2.22 = 21780 Pa = 21.78 kPa

Answer

Δp = 21.78 kPa
22.Pipe friction & head loss

Answer: H = 1.613 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 = 0.02/0.01767 = 1.132 m/s
V²/(2g) = 0.06529 m

Loss coefficients

f·L/D = 0.018·100/0.15 = 12
ΣK = 0.5 + 4·0.3 + 10 = 11.7

Energy equation

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

H = (1 + 12 + 11.7)·0.06529 = 1.613 m

Answer

H = 1.613 m
23.Pumps & pump power

Answer: Pshaft = 27.01 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.

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.03·78 = 22.96 kW

Shaft power

Pshaft = Ph/η = 22.96/0.85 = 27.01 kW

Answer

Pshaft = 27.01 kW
24.Pumps & pump power

Answer: Pshaft = 8.458 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 = 0.06/0.03142 = 1.91 m/s
V²/(2g) = 0.1859 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (15 + 3)·0.1859 = 3.346 m

Pump head

H = Δz + hL = 7 + 3.346 = 10.35 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.06·10.35/0.72 = 8.458 kW

Answer

Pshaft = 8.458 kW

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