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 1700 kg/h · 20% sugarStream 2ṁ₂ = ? · 35% sugarProduct25% sugar

How much of stream 2 must be added each hour to stream 1 so that the blended product contains 25% sugar? Find ṁ2.

ṁ1 = 700 kg/hx1 = 20 %x2 = 35 %x3 = 25 %
ṁ2 = kg/h
2.Mass balanceHard
EvaporatorFeed F2100 kg/h · 14% saltProduct P50% 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 = 2100 kg/hxF = 14 %xP = 50 %
W = kg/h
3.Energy balanceMedium
hot sidecold sideglycol mix · 180 °C140 °Cwater · 10 °Ct = ? °C

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

ṁh = 2.5 kg/scp,h = 3.6 kJ/(kg·K)Th: 180 → 140 °Cṁc = 3 kg/scp,c = 4.18 kJ/(kg·K)tin = 10 °C
tout = °C
4.Energy balanceHard
hot sidecold sideethanol · 140 °C70 °Cwater · 10 °C35 °C · ṁ = ?5% lost

Hot ethanol 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 = 2.44 kJ/(kg·K)Th: 140 → 70 °Ct: 10 → 35 °Ccp,c = 4.18 kJ/(kg·K)loss = 5 %
ṁc = kg/s
5.Ideal gas lawMedium
350 g of CO₂V = 50 LT = 60 °CP = ?

A tank of 50 L contains 350 g of CO₂ at 60 °C. Treat it as an ideal gas and find the pressure P.

m = 350 gM = 44.01 g/molV = 50 LT = 60 °CR = 8.314 J/(mol·K)
P = kPa
6.Ideal gas lawHard
CH₄, M = 16.04 g/molP = 500 kPaT = 170 °Cρ = ?

Find the density ρ of CH₄ at 500 kPa and 170 °C, treating it as an ideal gas.

M = 16.04 g/molP = 500 kPaT = 170 °CR = 8.314 J/(mol·K)
ρ = kg/m³
7.StoichiometryMedium
m(X)n(X)n(NaCl)m(NaCl)÷ M(X)× 2/ν× M(NaCl)

20 g of Na and 48 g of Cl2 react according to 2Na + Cl2 → 2NaCl. What mass m of NaCl can form?

M(Na) = 22.99M(Cl2) = 70.9M(NaCl) = 58.44 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, 6 g of Mg reacts completely (the other reactants are in excess) and 8.16 g of MgO is collected. Find the percent yield Y.

M(Mg) = 24.31 g/molM(MgO) = 40.3 g/molactual: 8.16 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 = 16. Find the equilibrium concentration [HI].

[H₂]₀ = [I₂]₀ = 0.4 mol/LKc = 16
[HI] = mol/L
10.Chemical equilibriumHard
PCl5​PCl3​Cl2​I0.200C−x+x+xE0.2 − xxx

PCl₅ decomposes: PCl₅ ⇌ PCl₃ + Cl₂, with Kc = 0.08 at the reaction temperature. A container starts with 0.2 mol/L of PCl₅ only. Find the equilibrium concentration [Cl2].

[PCl₅]₀ = 0.2 mol/LKc = 0.08
[Cl2] = mol/L
11.Calorimetry & enthalpyMedium
Tf​ = ?Copperm = 150 gT = 80 °Cc = 0.385 J/(g·°C)Waterm = 200 gT = 24 °Cc = 4.18 J/(g·°C)

A 150 g block of copper (c = 0.385 J/(g·°C)) at 80 °C is dropped into 200 g of water (c = 4.18 J/(g·°C)) at 24 °C in an insulated cup. Find the final temperature Tf.

mmetal = 150 gcmetal = 0.385 J/(g·°C)Tmetal = 80 °Cmwater = 200 gTwater = 24 °Ccwater = 4.18 J/(g·°C)
Tf = °C
12.Calorimetry & enthalpyHard
H250 g CH3​OH2CH3​OH + 3O₂reactants2CO₂ + 4H₂O(l)productsq = ?

Use the standard enthalpies of formation to find the heat q released when 250 g of CH3OH (M = 32.04 g/mol) burns completely: 2CH3OH + 3O₂ → 2CO₂ + 4H₂O(l). Give q as a positive number.

ΔH°f(CH3OH) = −238.7 kJ/molΔH°f(CO₂) = −393.5 kJ/molΔH°f(H₂O, l) = −285.8 kJ/molΔH°f(O₂) = 0
q = kJ
13.Reaction kineticsMedium
t (min)C (mol/L)15 min0.5

In a first-order reaction the concentration of A falls from 1 mol/L to 0.5 mol/L in 15 min. Find the rate constant k.

CA0 = 1 mol/LCA = 0.5 mol/Lt = 15 min
k = min⁻¹
14.Reaction kineticsHard
Tk25 °C0.140 °C?

A reaction has a rate constant of 0.1 min⁻¹ at 25 °C and an activation energy of 120 kJ/mol. Find the rate constant k2 at 40 °C.

k1 = 0.1 min⁻¹T1 = 25 °CT2 = 40 °CEa = 120 kJ/molR = 8.314 J/(mol·K)
k2 = min⁻¹
15.Reactor sizing (CSTR & PFR)Medium
QX = 95%same Q, k and X as the CSTR

A first-order liquid-phase reaction must reach 95% 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 = 95%first order, same k and Q
VCSTR/VPFR =
16.Reactor sizing (CSTR & PFR)Hard
V = 150 LV = 150 LQ = 20 L/minX = ?

A first-order liquid-phase reaction (k = 0.25 min⁻¹) runs in two equal CSTRs in series, each of 150 L. The feed rate is 20 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 = 20 L/mink = 0.25 min⁻¹
X = %
17.Heat exchangers (LMTD)Medium
lengthT125 °C80 °C10 °C35 °CΔT₁ΔT₂parallel flow

A parallel-flow heat exchanger transfers 300 kW. Its heat transfer area is 12 m². The hot fluid cools from 125 to 80 °C and the cold fluid heats from 10 to 35 °C. Find the overall heat transfer coefficient U.

Q̇ = 300 kWA = 12 m²Th: 125 → 80 °CTc: 10 → 35 °C
U = W/(m²·K)
18.Heat exchangers (LMTD)Hard
lengthT100 °C25 °C?ΔT₁ΔT₂condensing steam

Steam condenses at a constant 100 °C on the outside of the tubes of a condenser with a heat transfer area of 1.5 m² and U = 2500 W/(m²·K). Cooling water (1 kg/s, cp = 4.18 kJ/(kg·K)) enters the tubes at 25 °C. Find the water outlet temperature Tc,out.

Ts = 100 °CA = 1.5 m²U = 2500 W/(m²·K)ṁ = 1 kg/scp = 4.18 kJ/(kg·K)Tc,in = 25 °C
Tc,out = °C
19.Heat conductionMedium
Mineral wool, k = 0.04100 mmBrick, k = 0.72100 mm18 °C5 °CTi​ = ?Q̇

A wall is made of 100 mm of mineral wool and 100 mm of brick, with an area of 15 m². The outer faces are at 18 °C and 5 °C. Find the temperature Ti at the interface between the two layers.

L1 = 100 mm, k1 = 0.04 W/(m·K)L2 = 100 mm, k2 = 0.72 W/(m·K)A = 15 m²T1 = 18 °CT3 = 5 °C
Ti = °C
20.Heat conductionHard
Glass, k = 0.96150 mmConcrete, k = 1.4150 mmroom 21 °Coutside -10 °CQ̇

A wall of 150 mm glass and 150 mm concrete separates a room at 21 °C from outside air at -10 °C. The convection coefficients are 6 W/(m²·K) inside and 30 W/(m²·K) outside, and the wall area is 20 m². Find the overall heat transfer coefficient U of the wall.

L1 = 150 mm, k1 = 0.96 W/(m·K)L2 = 150 mm, k2 = 1.4 W/(m·K)A = 20 m²hi = 6 W/(m²·K)ho = 30 W/(m²·K)Troom = 21 °CTout = -10 °C
U = W/(m²·K)
21.Pipe friction & head lossMedium
Q = 15 L/sD = 100 mmL = 200 mf = 0.022

Water flows at 15 L/s through a pipe 200 m long with an inside diameter of 100 mm. Use the Darcy friction factor f = 0.022 and g = 9.81 m/s². Find the friction head loss hf.

Q = 15 L/sL = 200 mD = 100 mmf = 0.022g = 9.81 m/s²
hf = m
22.Pipe friction & head lossHard
K = 0.2Δz = 37 mL = 150 m, D = 150 mm, f = 0.0183× bend (K = 0.3)

Two open reservoirs are joined by a pipe 150 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.018. The water surface of the upper reservoir is 37 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each), a valve (K = 0.2) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². Find the flow rate Q in L/s.

Δz = 37 mL = 150 mD = 150 mmf = 0.018Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 0.2Kexit = 1.0
Q = L/s
23.Pumps & pump powerMedium
PQ = 20 L/sH = 14 m

A pump with an efficiency of 72% delivers 20 L/s of water (ρ = 1000 kg/m³) against a head of 14 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 20 L/sH = 14 mη = 72%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 75 L/sΔz = 8 mL = 150 m, D = 200 mm, f = 0.015, ΣK = 2.5

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 8 m higher. The pipe is 150 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.015; the minor-loss coefficients add up to ΣK = 2.5 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 80%. Find the shaft power Pshaft in kW.

Q = 75 L/sΔz = 8 mL = 150 mD = 200 mmf = 0.015ΣK = 2.5η = 80%
Pshaft = kW

3Solutions

1.Mass balance

Answer: ṁ2 = 350 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) = 700·(20 − 25)/(25 − 35) = 350 kg/h

Answer

ṁ2 = 350 kg/h
2.Mass balance

Answer: W = 1512 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 = 2100·14/50 = 588 kg/h

Total balance

W = F − P = 2100 − 588 = 1512 kg/h

Answer

W = 1512 kg/h
3.Energy balance

Answer: tout = 38.71 °C

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

Heat released by the hot stream

Q = 2.5·3.6·(180 − 140) = 360 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 10 + 360/(3·4.18) = 38.71 °C

Answer

tout = 38.71 °C
4.Energy balance

Answer: ṁc = 4.658 kg/s

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

Heat released

Qh = 3·2.44·(140 − 70) = 512.4 kW

Heat that reaches the water

Qc = (1 − 0.05)·512.4 = 486.8 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 486.8/(4.18·25) = 4.658 kg/s

Answer

ṁc = 4.658 kg/s
5.Ideal gas law

Answer: P = 440.6 kPa

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

Moles

n = m/M = 350/44.01 = 7.953 mol
T = 60 + 273.15 = 333.1 K

Pressure

P = nRT/V = 7.953·8.314·333.1/0.05 = 440.6 kPa

Answer

P = 440.6 kPa
6.Ideal gas law

Answer: ρ = 2.177 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 = 500·16.04/(8.314·443.1) = 2.177 kg/m³

Answer

ρ = 2.177 kg/m³
7.Stoichiometry

Answer: m = 50.84 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(Na) = 20/22.99 = 0.8699 mol
n(Cl2) = 48/70.9 = 0.677 mol

Limiting reactant

0.8699/2 = 0.435, 0.677/1 = 0.677 → Na

Mass of product

n(NaCl) = 0.435·2 = 0.8699 mol
m = 0.8699·58.44 = 50.84 g

Answer

m = 50.84 g
8.Stoichiometry

Answer: Y = 82.04 %

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) = 6/24.31 = 0.2468 mol
m = 0.2468·2/2·40.3 = 9.947 g

Percent yield

Y = 8.16/9.947·100 = 82.04%

Answer

Y = 82.04%
9.Chemical equilibrium

Answer: [HI] = 0.5333 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

16 = (2x)²/(0.4 − x)²

Take the square root

4 = 2x/(0.4 − x) → x = 0.4·4/(2 + 4) = 0.2667 mol/L

Equilibrium concentration

[HI] = 2x = 0.5333 mol/L

Answer

[HI] = 0.5333 mol/L
10.Chemical equilibrium

Answer: [Cl2] = 0.09266 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/(0.2 − x) → x² + 0.08·x − 0.016 = 0

Solve the quadratic

x = (−0.08 + √(0.08² + 4·0.016))/2 = 0.09266 mol/L

Equilibrium concentration

[Cl₂] = x = 0.09266 mol/L

Answer

[Cl2] = 0.09266 mol/L
11.Calorimetry & enthalpy

Answer: Tf = 27.62 °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

150·0.385·(80 − Tf) = 200·4.18·(Tf − 24)

Solve for the final temperature

Tf = (57.75·80 + 836·24)/(57.75 + 836) = 27.62 °C

Answer

Tf = 27.62 °C
12.Calorimetry & enthalpy

Answer: q = 5668 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) + 4·(−285.8)] − [2·(−238.7) + 3·0] = −1453 kJ

Heat for the given mass

n = 250/32.04 = 7.803 mol
q = n·|ΔH°/2| = 7.803·726.4 = 5668 kJ

Answer

q = 5668 kJ
13.Reaction kinetics

Answer: k = 0.04621 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(1/0.5)/15 = 0.6931/15 = 0.04621 min⁻¹

Answer

k = 0.04621 min⁻¹
14.Reaction kinetics

Answer: k2 = 1.016 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 = 313.1 K

Arrhenius ratio

ln(k2/k1) = −(120000/8.314)·(1/313.1 − 1/298.1) = 2.319
k2 = 0.1·e2.319 = 1.016 min⁻¹

Answer

k2 = 1.016 min⁻¹
15.Reactor sizing (CSTR & PFR)

Answer: VCSTR/VPFR = 6.342

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) = 0.95/0.05 = 19
PFR: k·τ = ln(1/(1 − X)) = ln(20) = 2.996

Ratio of volumes

VCSTR/VPFR = 19/2.996 = 6.342

Answer

VCSTR/VPFR = 6.342

The gap grows quickly at high conversion.

16.Reactor sizing (CSTR & PFR)

Answer: X = 87.9 %

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 = 0.25·7.5 = 1.875

Conversion

C1/CA0 = 1/(1 + kτ) = 1/(1 + 1.875) = 0.3478
C2/CA0 = 1/(1 + kτ)² = 0.121
X = 1 − 0.121 = 87.9%

Answer

X = 87.9%
17.Heat exchangers (LMTD)

Answer: U = 335.1 W/(m²·K)

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 − 10 = 115 K
ΔT₂ = Th,out − Tc,out = 80 − 35 = 45 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (115 − 45)/ln(115/45) = 74.61 K

Overall coefficient

U = Q̇/(A·ΔTlm) = 300000/(12·74.61) = 335.1 W/(m²·K)

Answer

U = 335.1 W/(m²·K)
18.Heat exchangers (LMTD)

Answer: Tc,out = 69.42 °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) = 2500·1.5/(1·4180) = 0.8971

Outlet temperature

ΔT₂ = ΔT₁·e−0.8971 = 75·0.4077 = 30.58 K
Tc,out = 100 − 30.58 = 69.42 °C

Answer

Tc,out = 69.42 °C

Heat transferred: Q̇ = 185.7 kW.

19.Heat conduction

Answer: Ti = 5.684 °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)/(0.04·15) = 0.1667 K/W
R2 = L2/(k2A) = (100/1000)/(0.72·15) = 0.009259 K/W

Heat flow

Q̇ = (T1 − T3)/(R1 + R2) = 13/0.1759 = 73.89 W

Interface temperature

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

Ti = T1 − Q̇·R1 = 18 − 73.89·0.1667 = 5.684 °C

Answer

Ti = 5.684 °C
20.Heat conduction

Answer: U = 2.158 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/(6·20) = 0.008333 K/W
R1 = L1/(k1A) = (150/1000)/(0.96·20) = 0.007813 K/W
R2 = L2/(k2A) = (150/1000)/(1.4·20) = 0.005357 K/W
Ro = 1/(hoA) = 1/(30·20) = 0.001667 K/W
ΣR = 0.02317 K/W

Overall coefficient

U = 1/(A·ΣR) = 1/(20·0.02317) = 2.158 W/(m²·K)

Answer

U = 2.158 W/(m²·K)
21.Pipe friction & head loss

Answer: hf = 8.18 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·0.1²/4 = 0.007854 m²
V = Q/A = 0.015/0.007854 = 1.91 m/s

Velocity head

V²/(2g) = 1.91²/(2·9.81) = 0.1859 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.022·(200/0.1)·1.91²/(2·9.81) = 8.18 m

Answer

hf = 8.18 m
22.Pipe friction & head loss

Answer: Q = 104.9 L/s

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.

Loss coefficients

f·L/D = 0.018·150/0.15 = 18
ΣK = 0.5 + 3·0.3 + 0.2 + 1.0 = 2.6

Energy equation

Both surfaces are open to the air and practically at rest, so all of Δz is lost in the pipe.

37 = (18 + 2.6)·V²/(2·9.81)
V = √(2·9.81·37/20.6) = 5.936 m/s

Flow rate

Q = V·π·D²/4 = 5.936·0.01767 = 0.1049 m³/s = 104.9 L/s

Answer

Q = 104.9 L/s
23.Pumps & pump power

Answer: Pshaft = 3.815 kW

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

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.02·14 = 2.747 kW

Shaft power

Pshaft = Ph/η = 2.747/0.72 = 3.815 kW

Answer

Pshaft = 3.815 kW
24.Pumps & pump power

Answer: Pshaft = 11.03 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 = 0.075/0.03142 = 2.387 m/s
V²/(2g) = 0.2905 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (11.25 + 2.5)·0.2905 = 3.994 m

Pump head

H = Δz + hL = 8 + 3.994 = 11.99 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.075·11.99/0.8 = 11.03 kW

Answer

Pshaft = 11.03 kW

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