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 1250 kg/h · 20% sugarStream 2ṁ₂ = ? · 40% sugarProduct30% sugar

How much of stream 2 must be added each hour to stream 1 so that the blended product contains 30% sugar? Find ṁ2.

ṁ1 = 250 kg/hx1 = 20 %x2 = 40 %x3 = 30 %
ṁ2 = kg/h
2.Mass balanceHard
EvaporatorFeed F4900 kg/h · 7% saltProduct PP = ? · 30%Vapour W (pure water)0% salt

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

F = 4900 kg/hxF = 7 %xP = 30 %
P = kg/h
3.Energy balanceMedium
hot sidecold sideethanol · 170 °C110 °Cwater · 10 °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: 170 → 110 °Cṁc = 3 kg/scp,c = 4.18 kJ/(kg·K)tin = 10 °C
tout = °C
4.Energy balanceHard
hot sidecold sidelight oil · 140 °C90 °Cwater · 15 °C85 °C · ṁ = ?15% lost

Hot light oil 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 = 3 kg/scp,h = 2.1 kJ/(kg·K)Th: 140 → 90 °Ct: 15 → 85 °Ccp,c = 4.18 kJ/(kg·K)loss = 15 %
ṁc = kg/s
5.Ideal gas lawMedium
40 g of N₂V = 10 LT = 20 °CP = ?

A tank of 10 L contains 40 g of N₂ at 20 °C. Treat it as an ideal gas and find the pressure P.

m = 40 gM = 28.01 g/molV = 10 LT = 20 °CR = 8.314 J/(mol·K)
P = kPa
6.Ideal gas lawHard
State 1State 2

A fixed amount of N₂ goes from 100 kPa, 20 L, 35 °C to 800 kPa and 50 °C. Find the new volume V2.

P1 = 100 kPaV1 = 20 LT1 = 35 °CP2 = 800 kPaT2 = 50 °C
V2 = L
7.StoichiometryMedium
m(X)n(X)n(AlCl3​)m(AlCl3​)÷ M(X)× 2/ν× M(AlCl3​)

20 g of Al and 32 g of Cl2 react according to 2Al + 3Cl2 → 2AlCl3. What mass m of AlCl3 can form?

M(Al) = 26.98M(Cl2) = 70.9M(AlCl3) = 133.33 g/mol
m = g
8.StoichiometryHard
m(Mg)n(Mg)n(MgO)m(MgO)÷ M(Mg)× 2/2× M(MgO)

In the reaction 2Mg + O2 → 2MgO, 12 g of Mg reacts completely (the other reactants are in excess) and 16.91 g of MgO is collected. Find the percent yield Y.

M(Mg) = 24.31 g/molM(MgO) = 40.3 g/molactual: 16.91 g
Y = %
9.Chemical equilibriumMedium
H2​I2​HII0.80.80C−x−x+2xE0.8 − x0.8 − x2x

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

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

PCl₅ decomposes: PCl₅ ⇌ PCl₃ + Cl₂, with Kc = 0.01 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 = 0.01
[Cl2] = mol/L
11.Calorimetry & enthalpyMedium
Tf​ = ?Leadm = 250 gT = 110 °Cc = 0.129 J/(g·°C)Waterm = 400 gT = 22 °Cc = 4.18 J/(g·°C)

A 250 g block of lead (c = 0.129 J/(g·°C)) at 110 °C is dropped into 400 g of water (c = 4.18 J/(g·°C)) at 22 °C in an insulated cup. Find the final temperature Tf.

mmetal = 250 gcmetal = 0.129 J/(g·°C)Tmetal = 110 °Cmwater = 400 gTwater = 22 °Ccwater = 4.18 J/(g·°C)
Tf = °C
12.Calorimetry & enthalpyHard
H50 g C6​H12​O6​C6​H12​O6​ + 6O₂reactants6CO₂ + 6H₂O(l)productsq = ?

Use the standard enthalpies of formation to find the heat q released when 50 g of C6H12O6 (M = 180.16 g/mol) burns completely: C6H12O6 + 6O₂ → 6CO₂ + 6H₂O(l). Give q as a positive number.

ΔH°f(C6H12O6) = −1274 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 = ?80%

A first-order reaction in a batch reactor has k = 0.1 min⁻¹. How long does it take to reach 80% conversion? Find t.

k = 0.1 min⁻¹X = 80 %
t = min
14.Reaction kineticsHard
Tk30 °C0.00250 °C0.0381

The rate constant of a reaction is 0.002 min⁻¹ at 30 °C and 0.0381 min⁻¹ at 50 °C. Find the activation energy Ea.

k1 = 0.002 min⁻¹T1 = 30 °Ck2 = 0.0381 min⁻¹T2 = 50 °CR = 8.314 J/(mol·K)
Ea = kJ/mol
15.Reactor sizing (CSTR & PFR)Medium
QX = 60%same Q, k and X as the CSTR

A first-order liquid-phase reaction must reach 60% conversion. How many times larger must a CSTR be than a PFR for the same feed rate, rate constant and conversion? Find the ratio VCSTR/VPFR.

X = 60%first order, same k and Q
VCSTR/VPFR =
16.Reactor sizing (CSTR & PFR)Hard
V = 1000 LV = 1000 LQ = 25 L/minX = ?

A first-order liquid-phase reaction (k = 0.2 min⁻¹) runs in two equal CSTRs in series, each of 1000 L. The feed rate is 25 L/min, the density is constant and the reactors are at steady state. Find the overall conversion X in percent.

V = 1000 L (×2)Q = 25 L/mink = 0.2 min⁻¹
X = %
17.Heat exchangers (LMTD)Medium
lengthT95 °C45 °C10 °C25 °CΔT₁ΔT₂parallel flow

A parallel-flow heat exchanger transfers 500 kW. The hot fluid cools from 95 to 45 °C and the cold fluid heats from 10 to 25 °C. The overall heat transfer coefficient is 200 W/(m²·K). Find the heat transfer area A needed.

Q̇ = 500 kWU = 200 W/(m²·K)Th: 95 → 45 °CTc: 10 → 25 °C
A = m²
18.Heat exchangers (LMTD)Hard
lengthT150 °C??15 °CΔT₁ΔT₂counter-flow

In a counter-flow heat exchanger both streams have the same heat capacity rate, ṁ·cp = 1.5 kW/K. The hot stream enters at 150 °C and the cold stream at 15 °C. The exchanger has A = 3 m² and U = 300 W/(m²·K). Find the hot outlet temperature Th,out.

Ch = Cc = 1.5 kW/KTh,in = 150 °CTc,in = 15 °CA = 3 m²U = 300 W/(m²·K)
Th,out = °C
19.Heat conductionMedium
Brick, k = 0.7250 mmMineral wool, k = 0.04150 mm15 °C4 °CTi​ = ?Q̇

A wall is made of 50 mm of brick and 150 mm of mineral wool, with an area of 15 m². The outer faces are at 15 °C and 4 °C. Find the temperature Ti at the interface between the two layers.

L1 = 50 mm, k1 = 0.72 W/(m·K)L2 = 150 mm, k2 = 0.04 W/(m·K)A = 15 m²T1 = 15 °CT3 = 4 °C
Ti = °C
20.Heat conductionHard
Mineral wool, k = 0.04100 mmGypsum board, k = 0.17150 mmroom 20 °Coutside -12 °CQ̇

A wall of 100 mm mineral wool and 150 mm gypsum board separates a room at 20 °C from outside air at -12 °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 overall heat transfer coefficient U of the wall.

L1 = 100 mm, k1 = 0.04 W/(m·K)L2 = 150 mm, k2 = 0.17 W/(m·K)A = 6 m²hi = 10 W/(m²·K)ho = 25 W/(m²·K)Troom = 20 °CTout = -12 °C
U = W/(m²·K)
21.Pipe friction & head lossMedium
V = 0.8 m/sD = 50 mmL = 500 mf = 0.025

Water (ρ = 1000 kg/m³) flows at 0.8 m/s through a horizontal pipe, 500 m long, with an inside diameter of 50 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 = 0.8 m/sL = 500 mD = 50 mmf = 0.025ρ = 1000 kg/m³
Δp = kPa
22.Pipe friction & head lossHard
K = 10free outletH = ?L = 300 m, D = 250 mm, f = 0.0252× bend (K = 0.3)

A pipe 300 m long with an inside diameter of 250 mm (Darcy friction factor f = 0.025) 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 = 10). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 120 L/s?

Q = 120 L/sL = 300 mD = 250 mmf = 0.025Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 10
H = m
23.Pumps & pump powerMedium
PQ = 100 L/sH = 46 m

In a test, a pump delivers 100 L/s of water (ρ = 1000 kg/m³) against a head of 46 m while its shaft takes 55 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 100 L/sH = 46 mPshaft = 55 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
200 kPa (gauge)PQ = 20 L/sΔz = 28 mL = 100 m, D = 100 mm, f = 0.018, ΣK = 6

A pump moves 20 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 28 m higher. The pipe is 100 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 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 200 kPa. Find the head H the pump must add.

Q = 20 L/sΔz = 28 mL = 100 mD = 100 mmf = 0.018ΣK = 6ptank = 200 kPa
H = m

3Solutions

1.Mass balance

Answer: ṁ2 = 250 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) = 250·(20 − 30)/(30 − 40) = 250 kg/h

Answer

ṁ2 = 250 kg/h
2.Mass balance

Answer: P = 1143 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 = 4900·7/30 = 1143 kg/h

Answer

P = 1143 kg/h
3.Energy balance

Answer: tout = 39.19 °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·(170 − 110) = 366 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 10 + 366/(3·4.18) = 39.19 °C

Answer

tout = 39.19 °C
4.Energy balance

Answer: ṁc = 0.9151 kg/s

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

Heat released

Qh = 3·2.1·(140 − 90) = 315 kW

Heat that reaches the water

Qc = (1 − 0.15)·315 = 267.8 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 267.8/(4.18·70) = 0.9151 kg/s

Answer

ṁc = 0.9151 kg/s
5.Ideal gas law

Answer: P = 348.1 kPa

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

Moles

n = m/M = 40/28.01 = 1.428 mol
T = 20 + 273.15 = 293.1 K

Pressure

P = nRT/V = 1.428·8.314·293.1/0.01 = 348.1 kPa

Answer

P = 348.1 kPa
6.Ideal gas law

Answer: V2 = 2.622 L

Combined gas law: for a fixed amount of ideal gas, P1V1/T1 = P2V2/T2.

Absolute temperatures

T1 = 308.1 K, T2 = 323.1 K

Combined gas law

V2 = V1·(P1/P2)·(T2/T1) = 20·(100/800)·(323.1/308.1) = 2.622 L

Answer

V2 = 2.622 L
7.Stoichiometry

Answer: m = 40.12 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(Al) = 20/26.98 = 0.7413 mol
n(Cl2) = 32/70.9 = 0.4513 mol

Limiting reactant

0.7413/2 = 0.3706, 0.4513/3 = 0.1504 → Cl2

Mass of product

n(AlCl3) = 0.1504·2 = 0.3009 mol
m = 0.3009·133.33 = 40.12 g

Answer

m = 40.12 g
8.Stoichiometry

Answer: Y = 85 %

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(Mg) = 12/24.31 = 0.4936 mol
m = 0.4936·2/2·40.3 = 19.89 g

Percent yield

Y = 16.91/19.89·100 = 85%

Answer

Y = 85%
9.Chemical equilibrium

Answer: [HI] = 1.28 mol/L

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

Equilibrium expression

64 = (2x)²/(0.8 − x)²

Take the square root

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

Equilibrium concentration

[HI] = 2x = 1.28 mol/L

Answer

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

Answer: [Cl2] = 0.02702 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/(0.1 − x) → x² + 0.01·x − 0.001 = 0

Solve the quadratic

x = (−0.01 + √(0.01² + 4·0.001))/2 = 0.02702 mol/L

Equilibrium concentration

[Cl₂] = x = 0.02702 mol/L

Answer

[Cl2] = 0.02702 mol/L
11.Calorimetry & enthalpy

Answer: Tf = 23.67 °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

250·0.129·(110 − Tf) = 400·4.18·(Tf − 22)

Solve for the final temperature

Tf = (32.25·110 + 1672·22)/(32.25 + 1672) = 23.67 °C

Answer

Tf = 23.67 °C
12.Calorimetry & enthalpy

Answer: q = 777.6 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° = [6·(−393.5) + 6·(−285.8)] − [1·(−1274) + 6·0] = −2802 kJ

Heat for the given mass

n = 50/180.16 = 0.2775 mol
q = n·|ΔH°/1| = 0.2775·2802 = 777.6 kJ

Answer

q = 777.6 kJ
13.Reaction kinetics

Answer: t = 16.09 min

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).

Conversion and concentration

C/C0 = 1 − X = 0.2

Solve for the time

t = −ln(1 − X)/k = −ln(0.2)/0.1 = 16.09 min

Answer

t = 16.09 min
14.Reaction kinetics

Answer: Ea = 120 kJ/mol

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 = 303.1 K, T2 = 323.1 K

Solve Arrhenius for Ea

Ea = −R·ln(k2/k1)/(1/T2 − 1/T1) = −8.314·2.947/(-2.042e-4) = 120014 J/mol
Ea = 120 kJ/mol

Answer

Ea = 120 kJ/mol
15.Reactor sizing (CSTR & PFR)

Answer: VCSTR/VPFR = 1.637

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

k·τ for each reactor

CSTR: k·τ = X/(1 − X) = 0.6/0.4 = 1.5
PFR: k·τ = ln(1/(1 − X)) = ln(2.5) = 0.9163

Ratio of volumes

VCSTR/VPFR = 1.5/0.9163 = 1.637

Answer

VCSTR/VPFR = 1.637

The gap grows quickly at high conversion.

16.Reactor sizing (CSTR & PFR)

Answer: X = 98.77 %

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

Space time

τ = V/Q = 1000/25 = 40 min, kτ = 0.2·40 = 8

Conversion

C1/CA0 = 1/(1 + kτ) = 1/(1 + 8) = 0.1111
C2/CA0 = 1/(1 + kτ)² = 0.01235
X = 1 − 0.01235 = 98.77%

Answer

X = 98.77%
17.Heat exchangers (LMTD)

Answer: A = 55.65 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 = 45 − 25 = 20 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (85 − 20)/ln(85/20) = 44.92 K

Area

A = Q̇/(U·ΔTlm) = 500000/(200·44.92) = 55.65 m²

Answer

A = 55.65 m²
18.Heat exchangers (LMTD)

Answer: Th,out = 99.38 °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.

Constant temperature difference

The cold outlet sits opposite the hot inlet: Tc,out = Tc,in + (Th,in − Th,out), so ΔT₁ = Th,in − Tc,out = Th,out − Tc,in = ΔT₂.

ΔTlm = Th,out − Tc,in

Energy balance equals rate equation

1.5·(150 − Th,out) = 0.9·(Th,out − 15)
Th,out = (1.5·150 + 0.9·15)/(1.5 + 0.9) = 99.38 °C

Answer

Th,out = 99.38 °C

Heat transferred: Q̇ = 75.94 kW; the cold stream leaves at 65.63 °C.

19.Heat conduction

Answer: Ti = 14.8 °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) = (50/1000)/(0.72·15) = 0.00463 K/W
R2 = L2/(k2A) = (150/1000)/(0.04·15) = 0.25 K/W

Heat flow

Q̇ = (T1 − T3)/(R1 + R2) = 11/0.2546 = 43.2 W

Interface temperature

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

Ti = T1 − Q̇·R1 = 15 − 43.2·0.00463 = 14.8 °C

Answer

Ti = 14.8 °C
20.Heat conduction

Answer: U = 0.2839 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/(10·6) = 0.01667 K/W
R1 = L1/(k1A) = (100/1000)/(0.04·6) = 0.4167 K/W
R2 = L2/(k2A) = (150/1000)/(0.17·6) = 0.1471 K/W
Ro = 1/(hoA) = 1/(25·6) = 0.006667 K/W
ΣR = 0.5871 K/W

Overall coefficient

U = 1/(A·ΣR) = 1/(6·0.5871) = 0.2839 W/(m²·K)

Answer

U = 0.2839 W/(m²·K)
21.Pipe friction & head loss

Answer: Δp = 80 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·(500/0.05)·0.8²/(2·9.81) = 8.155 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 = 1000·9.81·8.155 = 80000 Pa = 80 kPa

Answer

Δp = 80 kPa
22.Pipe friction & head loss

Answer: H = 12.82 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 = 0.12/0.04909 = 2.445 m/s
V²/(2g) = 0.3046 m

Loss coefficients

f·L/D = 0.025·300/0.25 = 30
ΣK = 0.5 + 2·0.3 + 10 = 11.1

Energy equation

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

H = (1 + 30 + 11.1)·0.3046 = 12.82 m

Answer

H = 12.82 m
23.Pumps & pump power

Answer: η = 82.05 %

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

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.1·46 = 45.13 kW

Efficiency

η = Ph/Pshaft = 45.13/55 = 82.05%

Answer

η = 82.05%
24.Pumps & pump power

Answer: H = 56.32 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 = 0.02/0.007854 = 2.546 m/s
V²/(2g) = 0.3305 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (18 + 6)·0.3305 = 7.932 m

Pressure head

p/(ρ·g) = 200000/(1000·9.81) = 20.39 m

Pump head

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

H = Δz + p/(ρ·g) + hL = 28 + 20.39 + 7.932 = 56.32 m

Answer

H = 56.32 m

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