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 1900 kg/h · 5% sugarStream 2ṁ₂ = ? · 30% sugarProduct20% sugar

How much of stream 2 must be added each hour to stream 1 so that the blended product contains 20% sugar? Find ṁ2.

ṁ1 = 900 kg/hx1 = 5 %x2 = 30 %x3 = 20 %
ṁ2 = kg/h
2.Mass balanceHard
EvaporatorFeed F4900 kg/h · 17% sugarProduct P30% 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 = 4900 kg/hxF = 17 %xP = 30 %
W = kg/h
3.Energy balanceMedium
hot sidecold sidelight oil · 130 °C80 °Cwater · 30 °Ct = ? °C

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

ṁh = 1.5 kg/scp,h = 2.1 kJ/(kg·K)Th: 130 → 80 °Cṁc = 1 kg/scp,c = 4.18 kJ/(kg·K)tin = 30 °C
tout = °C
4.Energy balanceHard
hot sidecold sidelight oil · 140 °C70 °Cwater · 20 °C40 °C · ṁ = ?10% lost

Hot light oil 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 kg/scp,h = 2.1 kJ/(kg·K)Th: 140 → 70 °Ct: 20 → 40 °Ccp,c = 4.18 kJ/(kg·K)loss = 10 %
ṁc = kg/s
5.Ideal gas lawMedium
450 g of HeV = 20 LT = 10 °CP = ?

A tank of 20 L contains 450 g of He at 10 °C. Treat it as an ideal gas and find the pressure P.

m = 450 gM = 4.003 g/molV = 20 LT = 10 °CR = 8.314 J/(mol·K)
P = kPa
6.Ideal gas lawHard
N₂, M = 28.01 g/molP = 200 kPaT = 40 °Cρ = ?

Find the density ρ of N₂ at 200 kPa and 40 °C, treating it as an ideal gas.

M = 28.01 g/molP = 200 kPaT = 40 °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​)

4 g of N2 and 64 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(Al)n(Al)n(AlCl3​)m(AlCl3​)÷ M(Al)× 2/2× M(AlCl3​)

In the reaction 2Al + 3Cl2 → 2AlCl3, 4 g of Al reacts completely (the other reactants are in excess) and 12.26 g of AlCl3 is collected. Find the percent yield Y.

M(Al) = 26.98 g/molM(AlCl3) = 133.33 g/molactual: 12.26 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 = 9. Find the equilibrium concentration [HI].

[H₂]₀ = [I₂]₀ = 0.4 mol/LKc = 9
[HI] = mol/L
10.Chemical equilibriumHard
PCl5​PCl3​Cl2​I100C−x+x+xE1 − xxx

PCl₅ decomposes: PCl₅ ⇌ PCl₃ + Cl₂, with Kc = 0.08 at the reaction temperature. A container starts with 1 mol/L of PCl₅ only. Find the equilibrium concentration [Cl2].

[PCl₅]₀ = 1 mol/LKc = 0.08
[Cl2] = mol/L
11.Calorimetry & enthalpyMedium
Tf​ = ?Aluminiumm = 100 gT = 90 °Cc = 0.897 J/(g·°C)Waterm = 300 gT = 18 °Cc = 4.18 J/(g·°C)

A 100 g block of aluminium (c = 0.897 J/(g·°C)) at 90 °C is dropped into 300 g of water (c = 4.18 J/(g·°C)) at 18 °C in an insulated cup. Find the final temperature Tf.

mmetal = 100 gcmetal = 0.897 J/(g·°C)Tmetal = 90 °Cmwater = 300 gTwater = 18 °Ccwater = 4.18 J/(g·°C)
Tf = °C
12.Calorimetry & enthalpyHard
HCH4​ + 2O₂reactantsCO₂ + 2H₂O(l)productsΔH° = ?

Use the standard enthalpies of formation to find ΔH° for the reaction CH4 + 2O₂ → CO₂ + 2H₂O(l).

ΔH°f(CH4) = −74.8 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)C (mol/L)15 min0.7

In a first-order reaction the concentration of A falls from 2 mol/L to 0.7 mol/L in 15 min. Find the rate constant k.

CA0 = 2 mol/LCA = 0.7 mol/Lt = 15 min
k = min⁻¹
14.Reaction kineticsHard
Tk25 °C0.00545 °C?

A reaction has a rate constant of 0.005 min⁻¹ at 25 °C and an activation energy of 80 kJ/mol. Find the rate constant k2 at 45 °C.

k1 = 0.005 min⁻¹T1 = 25 °CT2 = 45 °CEa = 80 kJ/molR = 8.314 J/(mol·K)
k2 = min⁻¹
15.Reactor sizing (CSTR & PFR)Medium
Q = 20 L/minX = 90%V = ?, k = 0.08 min⁻¹

A first-order liquid-phase reaction A → B with k = 0.08 min⁻¹ is carried out in a plug-flow reactor (PFR) fed at 20 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 = 20 L/mink = 0.08 min⁻¹X = 90%
V = L
16.Reactor sizing (CSTR & PFR)Hard
Q = 20 L/minX = ?V = 150 L

A first-order liquid-phase reaction (k = 0.3 min⁻¹) runs in a 150 L plug-flow reactor (PFR) fed at 20 L/min. The density is constant and the reactor is at steady state. Find the conversion X in percent.

V = 150 LQ = 20 L/mink = 0.3 min⁻¹
X = %
17.Heat exchangers (LMTD)Medium
lengthT95 °C80 °C10 °C25 °CΔT₁ΔT₂parallel flow

A parallel-flow heat exchanger transfers 480 kW. The hot fluid cools from 95 to 80 °C and the cold fluid heats from 10 to 25 °C. The overall heat transfer coefficient is 1000 W/(m²·K). Find the heat transfer area A needed.

Q̇ = 480 kWU = 1000 W/(m²·K)Th: 95 → 80 °CTc: 10 → 25 °C
A = m²
18.Heat exchangers (LMTD)Hard
lengthT100 °C45 °C17.57 °C10 °CΔT₁ΔT₂counter-flow

Hot oil (0.5 kg/s, cp = 2.3 kJ/(kg·K)) cools from 100 to 45 °C in a counter-flow exchanger. It heats 2 kg/s of water (cp = 4.18 kJ/(kg·K)) that enters at 10 °C. With U = 1000 W/(m²·K), find the heat transfer area A needed.

ṁh = 0.5 kg/scp,h = 2.3 kJ/(kg·K)Th: 100 → 45 °Cṁc = 2 kg/scp,c = 4.18 kJ/(kg·K)Tc,in = 10 °CU = 1000 W/(m²·K)
A = m²
19.Heat conductionMedium
Wood, k = 0.17150 mmGypsum board, k = 0.1750 mm15 °C-7 °CTi​ = ?Q̇

A wall is made of 150 mm of wood and 50 mm of gypsum board, with an area of 15 m². The outer faces are at 15 °C and -7 °C. Find the temperature Ti at the interface between the two layers.

L1 = 150 mm, k1 = 0.17 W/(m·K)L2 = 50 mm, k2 = 0.17 W/(m·K)A = 15 m²T1 = 15 °CT3 = -7 °C
Ti = °C
20.Heat conductionHard
Concrete, k = 1.4250 mmGypsum board, k = 0.1750 mmroom 20 °Coutside -7 °CTs​ = ?Q̇

A wall of 250 mm concrete and 50 mm gypsum board separates a room at 20 °C from outside air at -7 °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 temperature Ts of the inside surface of the wall.

L1 = 250 mm, k1 = 1.4 W/(m·K)L2 = 50 mm, k2 = 0.17 W/(m·K)A = 4 m²hi = 7.7 W/(m²·K)ho = 30 W/(m²·K)Troom = 20 °CTout = -7 °C
Ts = °C
21.Pipe friction & head lossMedium
Q = 3 L/sD = 75 mmL = 1000 mf = 0.015

Water flows at 3 L/s through a pipe 1000 m long with an inside diameter of 75 mm. Use the Darcy friction factor f = 0.015 and g = 9.81 m/s². Find the friction head loss hf.

Q = 3 L/sL = 1000 mD = 75 mmf = 0.015g = 9.81 m/s²
hf = m
22.Pipe friction & head lossHard
K = 10Δz = ?L = 100 m, D = 250 mm, f = 0.0184× bend (K = 0.3)

Two open reservoirs are joined by a pipe 100 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.018. The minor losses are a square-edged entrance (K = 0.5), 4 bends (K = 0.3 each), a valve (K = 10) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². What difference in water level Δz between the reservoirs gives a flow rate of 75 L/s?

Q = 75 L/sL = 100 mD = 250 mmf = 0.018Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 10Kexit = 1.0
Δz = m
23.Pumps & pump powerMedium
PQ = 50 L/sH = 12 m

In a test, a pump delivers 50 L/s of water (ρ = 1000 kg/m³) against a head of 12 m while its shaft takes 7.2 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 50 L/sH = 12 mPshaft = 7.2 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
PQ = 75 L/sΔz = 13 mL = 500 m, D = 250 mm, f = 0.02, ΣK = 8

A pump moves 75 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 13 m higher. The pipe is 500 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.02; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 75 L/sΔz = 13 mL = 500 mD = 250 mmf = 0.02ΣK = 8
H = m

3Solutions

1.Mass balance

Answer: ṁ2 = 1350 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) = 900·(5 − 20)/(20 − 30) = 1350 kg/h

Answer

ṁ2 = 1350 kg/h
2.Mass balance

Answer: W = 2123 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 = 4900·17/30 = 2777 kg/h

Total balance

W = F − P = 4900 − 2777 = 2123 kg/h

Answer

W = 2123 kg/h
3.Energy balance

Answer: tout = 67.68 °C

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

Heat released by the hot stream

Q = 1.5·2.1·(130 − 80) = 157.5 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 30 + 157.5/(1·4.18) = 67.68 °C

Answer

tout = 67.68 °C
4.Energy balance

Answer: ṁc = 3.165 kg/s

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

Heat released

Qh = 2·2.1·(140 − 70) = 294 kW

Heat that reaches the water

Qc = (1 − 0.1)·294 = 264.6 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 264.6/(4.18·20) = 3.165 kg/s

Answer

ṁc = 3.165 kg/s
5.Ideal gas law

Answer: P = 13232 kPa

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

Moles

n = m/M = 450/4.003 = 112.4 mol
T = 10 + 273.15 = 283.1 K

Pressure

P = nRT/V = 112.4·8.314·283.1/0.02 = 13232 kPa

Answer

P = 13232 kPa
6.Ideal gas law

Answer: ρ = 2.152 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 = 200·28.01/(8.314·313.1) = 2.152 kg/m³

Answer

ρ = 2.152 kg/m³
7.Stoichiometry

Answer: m = 4.862 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) = 4/28.02 = 0.1428 mol
n(H2) = 64/2.016 = 31.75 mol

Limiting reactant

0.1428/1 = 0.1428, 31.75/3 = 10.58 → N2

Mass of product

n(NH3) = 0.1428·2 = 0.2855 mol
m = 0.2855·17.03 = 4.862 g

Answer

m = 4.862 g
8.Stoichiometry

Answer: Y = 62.02 %

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(Al) = 4/26.98 = 0.1483 mol
m = 0.1483·2/2·133.33 = 19.77 g

Percent yield

Y = 12.26/19.77·100 = 62.02%

Answer

Y = 62.02%
9.Chemical equilibrium

Answer: [HI] = 0.48 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

9 = (2x)²/(0.4 − x)²

Take the square root

3 = 2x/(0.4 − x) → x = 0.4·3/(2 + 3) = 0.24 mol/L

Equilibrium concentration

[HI] = 2x = 0.48 mol/L

Answer

[HI] = 0.48 mol/L
10.Chemical equilibrium

Answer: [Cl2] = 0.2457 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

0.08 = x²/(1 − x) → x² + 0.08·x − 0.08 = 0

Solve the quadratic

x = (−0.08 + √(0.08² + 4·0.08))/2 = 0.2457 mol/L

Equilibrium concentration

[Cl₂] = x = 0.2457 mol/L

Answer

[Cl2] = 0.2457 mol/L
11.Calorimetry & enthalpy

Answer: Tf = 22.81 °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

100·0.897·(90 − Tf) = 300·4.18·(Tf − 18)

Solve for the final temperature

Tf = (89.7·90 + 1254·18)/(89.7 + 1254) = 22.81 °C

Answer

Tf = 22.81 °C
12.Calorimetry & enthalpy

Answer: ΔH° = −890.3 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° = [1·(−393.5) + 2·(−285.8)] − [1·(−74.8) + 2·0] = −890.3 kJ

Answer

ΔH° = −890.3 kJ

Negative: the reaction gives off heat (exothermic).

13.Reaction kinetics

Answer: k = 0.06999 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)/15 = 1.05/15 = 0.06999 min⁻¹

Answer

k = 0.06999 min⁻¹
14.Reaction kinetics

Answer: k2 = 0.03803 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 = 298.1 K, T2 = 318.1 K

Arrhenius ratio

ln(k2/k1) = −(80000/8.314)·(1/318.1 − 1/298.1) = 2.029
k2 = 0.005·e2.029 = 0.03803 min⁻¹

Answer

k2 = 0.03803 min⁻¹
15.Reactor sizing (CSTR & PFR)

Answer: V = 575.6 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))/0.08 = 2.303/0.08 = 28.78 min

Volume

V = Q·τ = 20·28.78 = 575.6 L

Answer

V = 575.6 L
16.Reactor sizing (CSTR & PFR)

Answer: X = 89.46 %

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 = 150/20 = 7.5 min, kτ = 0.3·7.5 = 2.25

Conversion

X = 1 − e−kτ = 1 − e−2.25 = 89.46%

Answer

X = 89.46%
17.Heat exchangers (LMTD)

Answer: A = 6.965 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 = 95 − 10 = 85 K
ΔT₂ = Th,out − Tc,out = 80 − 25 = 55 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (85 − 55)/ln(85/55) = 68.92 K

Area

A = Q̇/(U·ΔTlm) = 480000/(1000·68.92) = 6.965 m²

Answer

A = 6.965 m²
18.Heat exchangers (LMTD)

Answer: A = 1.142 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) = 0.5·2.3·55 = 63.25 kW
Tc,out = 10 + 63.25/(2·4.18) = 17.57 °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 = 100 − 17.57 = 82.43 K
ΔT₂ = Th,out − Tc,in = 45 − 10 = 35 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (82.43 − 35)/ln(82.43/35) = 55.37 K

Area

A = Q̇/(U·ΔTlm) = 63250/(1000·55.37) = 1.142 m²

Answer

A = 1.142 m²
19.Heat conduction

Answer: Ti = −1.5 °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) = (150/1000)/(0.17·15) = 0.05882 K/W
R2 = L2/(k2A) = (50/1000)/(0.17·15) = 0.01961 K/W

Heat flow

Q̇ = (T1 − T3)/(R1 + R2) = 22/0.07843 = 280.5 W

Interface temperature

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

Ti = T1 − Q̇·R1 = 15 − 280.5·0.05882 = −1.5 °C

Answer

Ti = −1.5 °C
20.Heat conduction

Answer: Ts = 14.49 °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.

Resistances in series

Ri = 1/(hiA) = 1/(7.7·4) = 0.03247 K/W
R1 = L1/(k1A) = (250/1000)/(1.4·4) = 0.04464 K/W
R2 = L2/(k2A) = (50/1000)/(0.17·4) = 0.07353 K/W
Ro = 1/(hoA) = 1/(30·4) = 0.008333 K/W
ΣR = 0.159 K/W

Heat loss

Q̇ = (20 − (-7))/0.159 = 169.8 W
Ts = Troom − Q̇·Ri = 20 − 169.8·0.03247 = 14.49 °C

Answer

Ts = 14.49 °C
21.Pipe friction & head loss

Answer: hf = 4.701 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.

Mean velocity

A = π·0.075²/4 = 0.004418 m²
V = Q/A = 0.003/0.004418 = 0.6791 m/s

Velocity head

V²/(2g) = 0.6791²/(2·9.81) = 0.0235 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.015·(1000/0.075)·0.6791²/(2·9.81) = 4.701 m

Answer

hf = 4.701 m
22.Pipe friction & head loss

Answer: Δz = 2.368 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 = 0.075/0.04909 = 1.528 m/s
V²/(2g) = 0.119 m

Loss coefficients

f·L/D = 0.018·100/0.25 = 7.2
ΣK = 0.5 + 4·0.3 + 10 + 1.0 = 12.7

Total head loss

hf = 7.2·0.119 = 0.8567 m
hm = 12.7·0.119 = 1.511 m
Δz = hf + hm = 2.368 m

Answer

Δz = 2.368 m
23.Pumps & pump power

Answer: η = 81.75 %

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 = 1000·9.81·0.05·12 = 5.886 kW

Efficiency

η = Ph/Pshaft = 5.886/7.2 = 81.75%

Answer

η = 81.75%
24.Pumps & pump power

Answer: H = 18.71 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 = 0.075/0.04909 = 1.528 m/s
V²/(2g) = 0.119 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (40 + 8)·0.119 = 5.711 m

Pump head

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

H = Δz + hL = 13 + 5.711 = 18.71 m

Answer

H = 18.71 m

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