FE Chemical exam practice: cram pack

Formula sheets, the key method steps for every topic and 24 practice problems, with full solutions at the back.

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1Formulas and methods

Mass balance

Steady state
in = out
Total balance
ṁ1 + ṁ2 = ṁ3
Component balance
ṁ1x1 + ṁ2x2 = ṁ3x3
Evaporator
F·xF = P·xP, W = F − P

Energy balance

Sensible heat
Q = ṁ·cp·ΔT
Latent heat
Q = ṁ·hfg
Mixing
ΣṁcpTin = ΣṁcpTout
Water
cp ≈ 4.18 kJ/(kg·K)

Ideal gas law

Ideal gas law
pV = nRT
Gas constant
R = 8.314 J/(mol·K)
Combined gas law
p1V1/T1 = p2V2/T2
Moles
n = m/M
Temperature
T[K] = T[°C] + 273.15

Stoichiometry

Moles
n = m/M
Concentration
c = n/V
Mole ratio
use the coefficients of the balanced equation
Limiting reactant
the one that runs out first
Percent yield
actual / theoretical × 100%

Method

  1. Write and balance the chemical equation.
  2. Convert the given mass to moles: n = m/M.
  3. Use the coefficients as the mole ratio to find the moles of the substance you want.
  4. Convert back to mass with m = n·M. With two reactants, find the limiting reactant first.

Chemical equilibrium

Equilibrium constant
Kc = [C]c[D]d/([A]a[B]b)
ICE table
Initial, Change (×coefficient), Equilibrium
Quadratic
x = (−b + √(b² − 4ac))/(2a)

Method

  1. Write Kc with products over reactants, each raised to the power of its coefficient.
  2. Set up an ICE table: Initial, Change (in steps of x times the coefficients), Equilibrium.
  3. Put the equilibrium expressions into Kc and solve for x.
  4. Check whether x is small enough for an approximation; otherwise solve the quadratic.

Calorimetry & enthalpy

Heat
q = m·c·ΔT
Water
c = 4.18 J/(g·°C)
Calorimeter
heat lost = heat gained
Enthalpy of reaction
ΔH° = ΣΔH°f(products) − ΣΔH°f(reactants)

Reaction kinetics

First order
ln(CA/CA0) = −kt
Half-life (first order)
t½ = ln 2/k
Second order
1/CA = 1/CA0 + kt
Arrhenius
k = A·e−Ea/(RT)
Two temperatures
ln(k2/k1) = (Ea/R)(1/T1 − 1/T2)

Reactor sizing (CSTR & PFR)

Space time
τ = V/Q
CSTR, first order
τ = X/(k·(1 − X)), CA = CA0/(1 + kτ)
PFR, first order
τ = ln(1/(1 − X))/k, CA = CA0·e−kτ
Conversion from volume
CSTR: X = kτ/(1 + kτ), PFR: X = 1 − e−kτ
N equal CSTRs in series
X = 1 − 1/(1 + kτi)N

Heat exchangers (LMTD)

Heat duty
Q = U·A·ΔTlm
Log mean temperature difference
ΔTlm = (ΔT1 − ΔT2)/ln(ΔT1/ΔT2)
Stream balance
Q = ṁcp(Tin − Tout)

Heat conduction

Fourier’s law
Q̇ = kAΔT/L
Conduction resistance
R = L/(kA)
Convection resistance
R = 1/(hA)
Resistances in series
Q̇ = ΔTtotal/ΣR
U-value
U = 1/(ΣR·A)

Pipe friction & head loss

Reynolds number
Re = V·D/ν = ρ·V·D/μ
Flow regime
laminar below Re ≈ 2000, turbulent above Re ≈ 4000
Mean velocity
V = Q/A, A = π·D²/4
Darcy–Weisbach
hf = f·(L/D)·V²/(2g)
Minor losses
hm = ΣK·V²/(2g)
Typical K values
entrance 0.5, exit 1.0, 90° bend ≈ 0.3
Pressure drop
Δp = ρ·g·hf
Two open reservoirs
Δz = (f·L/D + ΣK)·V²/(2g)
Free outlet
H = (1 + f·L/D + ΣK)·V²/(2g)

Pumps & pump power

Hydraulic power
Ph = ρ·g·Q·H = Q·Δp
Shaft power
Pshaft = Ph/ηpump
Electrical power
Pel = Pshaft/ηmotor
Pump head
H = Δz + Δp/(ρ·g) + hL
System losses
hL = (f·L/D + ΣK)·V²/(2g)

2Practice problems

1.Mass balanceMedium
MixerStream 1550 kg/h · 35% sugarStream 2ṁ₂ = ? · 20% 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 = 550 kg/hx1 = 35 %x2 = 20 %x3 = 25 %
ṁ2 = kg/h
2.Mass balanceHard
EvaporatorFeed F4000 kg/h · 11% saltProduct PP = ? · 45%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 = 4000 kg/hxF = 11 %xP = 45 %
P = kg/h
3.Energy balanceMedium
hot sidecold sidelight oil · 180 °C130 °Cwater · 20 °Ct = ? °C

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

ṁh = 2.5 kg/scp,h = 2.1 kJ/(kg·K)Th: 180 → 130 °Cṁc = 1 kg/scp,c = 4.18 kJ/(kg·K)tin = 20 °C
tout = °C
4.Energy balanceHard
hot sidecold sideglycol mix · 120 °C60 °Cwater · 10 °C80 °C · ṁ = ?15% lost

Hot glycol mix 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 = 3.6 kJ/(kg·K)Th: 120 → 60 °Ct: 10 → 80 °Ccp,c = 4.18 kJ/(kg·K)loss = 15 %
ṁc = kg/s
5.Ideal gas lawMedium
400 g of ArP = 150 kPaT = 35 °CV = ?

What volume V does 400 g of Ar occupy at 150 kPa and 35 °C? Treat it as an ideal gas.

m = 400 gM = 39.95 g/molP = 150 kPaT = 35 °CR = 8.314 J/(mol·K)
V = L
6.Ideal gas lawHard
O₂, M = 32 g/molP = 450 kPaT = 10 °Cρ = ?

Find the density ρ of O₂ at 450 kPa and 10 °C, treating it as an ideal gas.

M = 32 g/molP = 450 kPaT = 10 °CR = 8.314 J/(mol·K)
ρ = kg/m³
7.StoichiometryMedium
m(X)n(X)n(H2​O)m(H2​O)÷ M(X)× 2/ν× M(H2​O)

6 g of H2 and 80 g of O2 react according to 2H2 + O2 → 2H2O. What mass m of H2O can form?

M(H2) = 2.016M(O2) = 32M(H2O) = 18.02 g/mol
m = g
8.StoichiometryHard
m(N2​)n(N2​)n(NH3​)m(NH3​)÷ M(N2​)× 2/1× M(NH3​)

In the reaction N2 + 3H2 → 2NH3, 4 g of N2 reacts completely (the other reactants are in excess) and 4.42 g of NH3 is collected. Find the percent yield Y.

M(N2) = 28.02 g/molM(NH3) = 17.03 g/molactual: 4.42 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 = 54. Find the equilibrium concentration [HI].

[H₂]₀ = [I₂]₀ = 0.8 mol/LKc = 54
[HI] = mol/L
10.Chemical equilibriumHard
PCl5​PCl3​Cl2​I0.2500C−x+x+xE0.25 − xxx

PCl₅ decomposes: PCl₅ ⇌ PCl₃ + Cl₂, with Kc = 0.08 at the reaction temperature. A container starts with 0.25 mol/L of PCl₅ only. Find the equilibrium concentration [PCl5].

[PCl₅]₀ = 0.25 mol/LKc = 0.08
[PCl5] = mol/L
11.Calorimetry & enthalpyMedium
Tf​ = ?Aluminiumm = 200 gT = 120 °Cc = 0.897 J/(g·°C)Waterm = 200 gT = 21 °Cc = 4.18 J/(g·°C)

A 200 g block of aluminium (c = 0.897 J/(g·°C)) at 120 °C is dropped into 200 g of water (c = 4.18 J/(g·°C)) at 21 °C in an insulated cup. Find the final temperature Tf.

mmetal = 200 gcmetal = 0.897 J/(g·°C)Tmetal = 120 °Cmwater = 200 gTwater = 21 °Ccwater = 4.18 J/(g·°C)
Tf = °C
12.Calorimetry & enthalpyHard
H250 g C6​H12​O6​C6​H12​O6​ + 6O₂reactants6CO₂ + 6H₂O(l)productsq = ?

Use the standard enthalpies of formation to find the heat q released when 250 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 second-order reaction (−rA = k·CA²) in a batch reactor has k = 0.2 L/(mol·min) and starts at 0.5 mol/L. How long does it take to reach 80% conversion? Find t.

k = 0.2 L/(mol·min)CA0 = 0.5 mol/LX = 80 %
t = min
14.Reaction kineticsHard
CA0​ (mol/L)r (mol/(L·s))run 10.40.005run 20.80.02n = ?

Two experiments measure the initial rate of A → products. With CA0 = 0.4 mol/L the rate is 0.005 mol/(L·s); with CA0 = 0.8 mol/L it is 0.02 mol/(L·s). Find the reaction order n with respect to A.

CA0,1 = 0.4 mol/Lr1 = 0.005 mol/(L·s)CA0,2 = 0.8 mol/Lr2 = 0.02 mol/(L·s)
n =
15.Reactor sizing (CSTR & PFR)Medium
Q = 10 L/minCA0​ = 0.5 mol/LCA​ = ?V = 150 L, k = 0.25 min⁻¹

A liquid-phase first-order reaction A → B (k = 0.25 min⁻¹) runs in a 150 L plug-flow reactor (PFR). The feed enters at 10 L/min with CA0 = 0.5 mol/L. The density is constant and the reactor is at steady state. Find the outlet concentration CA.

V = 150 LQ = 10 L/mink = 0.25 min⁻¹CA0 = 0.5 mol/L
CA = mol/L
16.Reactor sizing (CSTR & PFR)Hard
V = 150 LV = 150 LQ = 80 L/minX = ?

A first-order liquid-phase reaction (k = 0.3 min⁻¹) runs in two equal CSTRs in series, each of 150 L. The feed rate is 80 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 = 80 L/mink = 0.3 min⁻¹
X = %
17.Heat exchangers (LMTD)Medium
lengthT80 °C65 °C10 °C50 °CΔT₁ΔT₂parallel flow

A parallel-flow heat exchanger transfers 300 kW. Its heat transfer area is 4 m². The hot fluid cools from 80 to 65 °C and the cold fluid heats from 10 to 50 °C. Find the overall heat transfer coefficient U.

Q̇ = 300 kWA = 4 m²Th: 80 → 65 °CTc: 10 → 50 °C
U = W/(m²·K)
18.Heat exchangers (LMTD)Hard
lengthT160 °C120 °C?10 °CΔT₁ΔT₂counter-flow

In a counter-flow double-pipe heat exchanger, hot oil (1 kg/s, cp = 2.5 kJ/(kg·K)) flows in the inner tube and cools from 160 to 120 °C. Water (0.5 kg/s, cp = 4.18 kJ/(kg·K)) in the annulus enters at 10 °C. The inner tube has a diameter of 32 mm, and U = 500 W/(m²·K) is based on this diameter. Find the tube length L needed.

ṁh = 1 kg/scp,h = 2.5 kJ/(kg·K)Th: 160 → 120 °Cṁc = 0.5 kg/sTc,in = 10 °CD = 32 mmU = 500 W/(m²·K)
L = m
19.Heat conductionMedium
Wood, k = 0.17200 mmConcrete, k = 1.4150 mm19 °C-11 °CTi​ = ?Q̇

A wall is made of 200 mm of wood and 150 mm of concrete, with an area of 12 m². The outer faces are at 19 °C and -11 °C. Find the temperature Ti at the interface between the two layers.

L1 = 200 mm, k1 = 0.17 W/(m·K)L2 = 150 mm, k2 = 1.4 W/(m·K)A = 12 m²T1 = 19 °CT3 = -11 °C
Ti = °C
20.Heat conductionHard
Expanded polystyrene, k = 0.035250 mmGlass, k = 0.9675 mmroom 20 °Coutside 3 °CQ̇ = ?

A wall of 250 mm expanded polystyrene and 75 mm glass separates a room at 20 °C from outside air at 3 °C. The convection coefficients are 7.7 W/(m²·K) inside and 20 W/(m²·K) outside, and the wall area is 12 m². Find the heat loss Q̇ through the wall.

L1 = 250 mm, k1 = 0.035 W/(m·K)L2 = 75 mm, k2 = 0.96 W/(m·K)A = 12 m²hi = 7.7 W/(m²·K)ho = 20 W/(m²·K)Troom = 20 °CTout = 3 °C
Q̇ = W
21.Pipe friction & head lossMedium
Q = 75 L/sD = 300 mmL = 200 mf = 0.022

Water flows at 75 L/s through a pipe 200 m long with an inside diameter of 300 mm. Use the Darcy friction factor f = 0.022 and g = 9.81 m/s². Find the friction head loss hf.

Q = 75 L/sL = 200 mD = 300 mmf = 0.022g = 9.81 m/s²
hf = m
22.Pipe friction & head lossHard
K = 0.2free outletH = ?L = 200 m, D = 300 mm, f = 0.0224× bend (K = 0.3)

A pipe 200 m long with an inside diameter of 300 mm (Darcy friction factor f = 0.022) 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 = 0.2). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 100 L/s?

Q = 100 L/sL = 200 mD = 300 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 0.2
H = m
23.Pumps & pump powerMedium
PQ = 50 L/sH = 24 m

In a test, a pump delivers 50 L/s of water (ρ = 1000 kg/m³) against a head of 24 m while its shaft takes 14.4 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 50 L/sH = 24 mPshaft = 14.4 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
200 kPa (gauge)PQ = 100 L/sΔz = 17 mL = 300 m, D = 250 mm, f = 0.015, ΣK = 6

A pump moves 100 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 17 m higher. The pipe is 300 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.015; 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 = 100 L/sΔz = 17 mL = 300 mD = 250 mmf = 0.015ΣK = 6ptank = 200 kPa
H = m

3Solutions

1.Mass balance

Answer: ṁ2 = 1100 kg/h

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

Balances

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

Solve for ṁ2

ṁ2 = ṁ1(x1 − x3)/(x3 − x2) = 550·(35 − 25)/(25 − 20) = 1100 kg/h

Answer

ṁ2 = 1100 kg/h
2.Mass balance

Answer: P = 977.8 kg/h

Tie component: a component that passes through unchanged in one stream (here the solute) links the flows directly. Then the total balance gives the rest.

Solute balance

F·xF = P·xP → P = 4000·11/45 = 977.8 kg/h

Answer

P = 977.8 kg/h
3.Energy balance

Answer: tout = 82.8 °C

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

Heat released by the hot stream

Q = 2.5·2.1·(180 − 130) = 262.5 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 20 + 262.5/(1·4.18) = 82.8 °C

Answer

tout = 82.8 °C
4.Energy balance

Answer: ṁc = 1.882 kg/s

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

Heat released

Qh = 3·3.6·(120 − 60) = 648 kW

Heat that reaches the water

Qc = (1 − 0.15)·648 = 550.8 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 550.8/(4.18·70) = 1.882 kg/s

Answer

ṁc = 1.882 kg/s
5.Ideal gas law

Answer: V = 171 L

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

Moles

n = 400/39.95 = 10.01 mol
T = 35 + 273.15 = 308.1 K

Volume

V = nRT/P = 10.01·8.314·308.1/150 = 171 L

Answer

V = 171 L
6.Ideal gas law

Answer: ρ = 6.117 kg/m³

Ideal gas density: ρ = PM/(RT).

Rearrange the gas law

PV = (m/M)RT → ρ = m/V = PM/(RT)
T = 10 + 273.15 = 283.1 K

Density

ρ = 450·32/(8.314·283.1) = 6.117 kg/m³

Answer

ρ = 6.117 kg/m³
7.Stoichiometry

Answer: m = 53.63 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(H2) = 6/2.016 = 2.976 mol
n(O2) = 80/32 = 2.5 mol

Limiting reactant

2.976/2 = 1.488, 2.5/1 = 2.5 → H2

Mass of product

n(H2O) = 1.488·2 = 2.976 mol
m = 2.976·18.02 = 53.63 g

Answer

m = 53.63 g
8.Stoichiometry

Answer: Y = 90.9 %

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(N2) = 4/28.02 = 0.1428 mol
m = 0.1428·2/1·17.03 = 4.862 g

Percent yield

Y = 4.42/4.862·100 = 90.9%

Answer

Y = 90.9%
9.Chemical equilibrium

Answer: [HI] = 1.258 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

54 = (2x)²/(0.8 − x)²

Take the square root

7.348 = 2x/(0.8 − x) → x = 0.8·7.348/(2 + 7.348) = 0.6288 mol/L

Equilibrium concentration

[HI] = 2x = 1.258 mol/L

Answer

[HI] = 1.258 mol/L
10.Chemical equilibrium

Answer: [PCl5] = 0.143 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/(0.25 − x) → x² + 0.08·x − 0.02 = 0

Solve the quadratic

x = (−0.08 + √(0.08² + 4·0.02))/2 = 0.107 mol/L

Equilibrium concentration

[PCl₅] = 0.25 − 0.107 = 0.143 mol/L

Answer

[PCl5] = 0.143 mol/L
11.Calorimetry & enthalpy

Answer: Tf = 38.49 °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·(120 − Tf) = 200·4.18·(Tf − 21)

Solve for the final temperature

Tf = (179.4·120 + 836·21)/(179.4 + 836) = 38.49 °C

Answer

Tf = 38.49 °C
12.Calorimetry & enthalpy

Answer: q = 3888 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 = 250/180.16 = 1.388 mol
q = n·|ΔH°/1| = 1.388·2802 = 3888 kJ

Answer

q = 3888 kJ
13.Reaction kinetics

Answer: t = 40 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)/0.2 = 40 min

Answer

t = 40 min
14.Reaction kinetics

Answer: n = 2

Method of initial rates: for r = k·Cⁿ, comparing two runs that differ only in the starting concentration removes k: r₂/r₁ = (C₂/C₁)ⁿ. Doubling C doubles the rate for first order and quadruples it for second order.

Ratios

r2/r1 = 0.02/0.005 = 4
C2/C1 = 0.8/0.4 = 2

Order

n = ln(4)/ln(2) = 2

Answer

n = 2
15.Reactor sizing (CSTR & PFR)

Answer: CA = 0.01176 mol/L

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

Space time

τ = V/Q = 150/10 = 15 min

Outlet concentration

CA = 0.5·e−0.25·15 = 0.01176 mol/L

Answer

CA = 0.01176 mol/L

Conversion: X = 97.65%.

16.Reactor sizing (CSTR & PFR)

Answer: X = 59.04 %

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 = 150/80 = 1.875 min, kτ = 0.3·1.875 = 0.5625

Conversion

C1/CA0 = 1/(1 + kτ) = 1/(1 + 0.5625) = 0.64
C2/CA0 = 1/(1 + kτ)² = 0.4096
X = 1 − 0.4096 = 59.04%

Answer

X = 59.04%
17.Heat exchangers (LMTD)

Answer: U = 2101 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 = 80 − 10 = 70 K
ΔT₂ = Th,out − Tc,out = 65 − 50 = 15 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (70 − 15)/ln(70/15) = 35.7 K

Overall coefficient

U = Q̇/(A·ΔTlm) = 300000/(4·35.7) = 2101 W/(m²·K)

Answer

U = 2101 W/(m²·K)
18.Heat exchangers (LMTD)

Answer: L = 18.76 m

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 = 1·2.5·(160 − 120) = 100 kW
Tc,out = 10 + 100/(0.5·4.18) = 57.85 °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 = 160 − 57.85 = 102.2 K
ΔT₂ = Th,out − Tc,in = 120 − 10 = 110 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (102.2 − 110)/ln(102.2/110) = 106 K

Area and length

A = 100000/(500·106) = 1.886 m²
L = A/(πD) = 1.886/(π·0.032) = 18.76 m

Answer

L = 18.76 m
19.Heat conduction

Answer: Ti = −8.496 °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) = (200/1000)/(0.17·12) = 0.09804 K/W
R2 = L2/(k2A) = (150/1000)/(1.4·12) = 0.008929 K/W

Heat flow

Q̇ = (T1 − T3)/(R1 + R2) = 30/0.107 = 280.5 W

Interface temperature

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

Ti = T1 − Q̇·R1 = 19 − 280.5·0.09804 = −8.496 °C

Answer

Ti = −8.496 °C
20.Heat conduction

Answer: Q̇ = 27.56 W

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/(7.7·12) = 0.01082 K/W
R1 = L1/(k1A) = (250/1000)/(0.035·12) = 0.5952 K/W
R2 = L2/(k2A) = (75/1000)/(0.96·12) = 0.00651 K/W
Ro = 1/(hoA) = 1/(20·12) = 0.004167 K/W
ΣR = 0.6167 K/W

Heat loss

Q̇ = (20 − (3))/0.6167 = 27.56 W

Answer

Q̇ = 27.56 W
21.Pipe friction & head loss

Answer: hf = 0.8416 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·0.3²/4 = 0.07069 m²
V = Q/A = 0.075/0.07069 = 1.061 m/s

Velocity head

V²/(2g) = 1.061²/(2·9.81) = 0.05738 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.022·(200/0.3)·1.061²/(2·9.81) = 0.8416 m

Answer

hf = 0.8416 m
22.Pipe friction & head loss

Answer: H = 1.792 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 = 0.1/0.07069 = 1.415 m/s
V²/(2g) = 0.102 m

Loss coefficients

f·L/D = 0.022·200/0.3 = 14.67
ΣK = 0.5 + 4·0.3 + 0.2 = 1.9

Energy equation

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

H = (1 + 14.67 + 1.9)·0.102 = 1.792 m

Answer

H = 1.792 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 = 1000·9.81·0.05·24 = 11.77 kW

Efficiency

η = Ph/Pshaft = 11.77/14.4 = 81.75%

Answer

η = 81.75%
24.Pumps & pump power

Answer: H = 42.46 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 = 0.1/0.04909 = 2.037 m/s
V²/(2g) = 0.2115 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (18 + 6)·0.2115 = 5.077 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 = 17 + 20.39 + 5.077 = 42.46 m

Answer

H = 42.46 m

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