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 11000 kg/h · 40% saltStream 2ṁ₂ = ? · 10% saltProduct15% salt

How much of stream 2 must be added each hour to stream 1 so that the blended product contains 15% salt? Find ṁ2.

ṁ1 = 1000 kg/hx1 = 40 %x2 = 10 %x3 = 15 %
ṁ2 = kg/h
2.Mass balanceHard
EvaporatorFeed F4700 kg/h · 19% saltProduct P65% 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 = 4700 kg/hxF = 19 %xP = 65 %
W = kg/h
3.Energy balanceMedium
hot sidecold sidelight oil · 180 °C130 °Cwater · 10 °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 = 2 kg/scp,c = 4.18 kJ/(kg·K)tin = 10 °C
tout = °C
4.Energy balanceHard
hot sidecold sideethanol · 120 °C90 °Cwater · 10 °C55 °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 = 1.5 kg/scp,h = 2.44 kJ/(kg·K)Th: 120 → 90 °Ct: 10 → 55 °Ccp,c = 4.18 kJ/(kg·K)loss = 5 %
ṁc = kg/s
5.Ideal gas lawMedium
80 g of ArV = 50 LT = 5 °CP = ?

A tank of 50 L contains 80 g of Ar at 5 °C. Treat it as an ideal gas and find the pressure P.

m = 80 gM = 39.95 g/molV = 50 LT = 5 °CR = 8.314 J/(mol·K)
P = kPa
6.Ideal gas lawHard
He, M = 4.003 g/molP = 750 kPaT = 130 °Cρ = ?

Find the density ρ of He at 750 kPa and 130 °C, treating it as an ideal gas.

M = 4.003 g/molP = 750 kPaT = 130 °CR = 8.314 J/(mol·K)
ρ = kg/m³
7.StoichiometryMedium
m(X)n(X)n(MgO)m(MgO)÷ M(X)× 2/ν× M(MgO)

20 g of Mg and 64 g of O2 react according to 2Mg + O2 → 2MgO. What mass m of MgO can form?

M(Mg) = 24.31M(O2) = 32M(MgO) = 40.3 g/mol
m = g
8.StoichiometryHard
m(C6​H12​O6​)n(C6​H12​O6​)n(C2​H5​OH)m(C2​H5​OH)÷ M(C6​H12​O6​)× 2/1× M(C2​H5​OH)

In the reaction C6H12O6 → 2C2H5OH + 2CO2, 24 g of C6H12O6 reacts completely (the other reactants are in excess) and 9.57 g of C2H5OH is collected. Find the percent yield Y.

M(C6H12O6) = 180.16 g/molM(C2H5OH) = 46.07 g/molactual: 9.57 g
Y = %
9.Chemical equilibriumMedium
H2​I2​HII0.20.20C−x−x+2xE0.2 − x0.2 − x2x

0.2 mol/L of H₂ and 0.2 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 = 0.2 mol/LKc = 9
[HI] = mol/L
10.Chemical equilibriumHard
PCl5​PCl3​Cl2​I0.2500C−x+x+xE0.25 − xxx

PCl₅ decomposes: PCl₅ ⇌ PCl₃ + Cl₂, with Kc = 0.05 at the reaction temperature. A container starts with 0.25 mol/L of PCl₅ only. Find the equilibrium concentration [Cl2].

[PCl₅]₀ = 0.25 mol/LKc = 0.05
[Cl2] = mol/L
11.Calorimetry & enthalpyMedium
Tf​ = ?Zincm = 250 gT = 90 °Cc = 0.388 J/(g·°C)Waterm = 400 gT = 20 °Cc = 4.18 J/(g·°C)

A 250 g block of zinc (c = 0.388 J/(g·°C)) at 90 °C is dropped into 400 g of water (c = 4.18 J/(g·°C)) at 20 °C in an insulated cup. Find the final temperature Tf.

mmetal = 250 gcmetal = 0.388 J/(g·°C)Tmetal = 90 °Cmwater = 400 gTwater = 20 °Ccwater = 4.18 J/(g·°C)
Tf = °C
12.Calorimetry & enthalpyHard
HC6​H12​O6​ + 6O₂reactants6CO₂ + 6H₂O(l)productsΔH° = ?

Use the standard enthalpies of formation to find ΔH° for the reaction C6H12O6 + 6O₂ → 6CO₂ + 6H₂O(l).

ΔH°f(C6H12O6) = −1274 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)t½​ = ?C0​/2

A second-order reaction (−rA = k·CA²) has k = 0.4 L/(mol·min) and an initial concentration of 0.5 mol/L. Find its first half-life t½.

k = 0.4 L/(mol·min)CA0 = 0.5 mol/L
t½ = min
14.Reaction kineticsHard
Tk40 °Ck1​?2·k1​

A reaction has an activation energy of 50 kJ/mol. At 40 °C it is too slow. To what temperature T2 (in °C) must it be heated to make it 2 times faster?

Ea = 50 kJ/molT1 = 40 °Ck2/k1 = 2R = 8.314 J/(mol·K)
T2 = °C
15.Reactor sizing (CSTR & PFR)Medium
QX = 85%same Q, k and X as the CSTR

A first-order liquid-phase reaction must reach 85% 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 = 85%first order, same k and Q
VCSTR/VPFR =
16.Reactor sizing (CSTR & PFR)Hard
Q = 80 L/minX = ?V = 200 L

A first-order liquid-phase reaction (k = 0.15 min⁻¹) runs in a 200 L plug-flow reactor (PFR) fed at 80 L/min. The density is constant and the reactor is at steady state. Find the conversion X in percent.

V = 200 LQ = 80 L/mink = 0.15 min⁻¹
X = %
17.Heat exchangers (LMTD)Medium
lengthT145 °C55 °C60 °C30 °CΔT₁ΔT₂counter-flow

A shell-and-tube heat exchanger (one shell pass, two tube passes) must transfer 610 kW. The hot fluid cools from 145 to 55 °C and the cold fluid heats from 30 to 60 °C. The LMTD correction factor for this arrangement is F = 0.8, and U = 1000 W/(m²·K). Find the heat transfer area A needed.

Q̇ = 610 kWF = 0.8U = 1000 W/(m²·K)Th: 145 → 55 °CTc: 30 → 60 °C
A = m²
18.Heat exchangers (LMTD)Hard
lengthT115 °C95 °C20.05 °C10 °CΔT₁ΔT₂counter-flow

Hot oil (1 kg/s, cp = 2.1 kJ/(kg·K)) cools from 115 to 95 °C in a counter-flow exchanger. It heats 1 kg/s of water (cp = 4.18 kJ/(kg·K)) that enters at 10 °C. With U = 500 W/(m²·K), find the heat transfer area A needed.

ṁh = 1 kg/scp,h = 2.1 kJ/(kg·K)Th: 115 → 95 °Cṁc = 1 kg/scp,c = 4.18 kJ/(kg·K)Tc,in = 10 °CU = 500 W/(m²·K)
A = m²
19.Heat conductionMedium
Gypsum board, k = 0.1750 mmGlass, k = 0.96150 mm17 °C-7 °CQ̇ = ?

A wall is made of 50 mm of gypsum board and 150 mm of glass, with an area of 10 m². The outer faces are at 17 °C and -7 °C. Find the heat flow Q̇ through the wall.

L1 = 50 mm, k1 = 0.17 W/(m·K)L2 = 150 mm, k2 = 0.96 W/(m·K)A = 10 m²T1 = 17 °CT3 = -7 °C
Q̇ = W
20.Heat conductionHard
Concrete, k = 1.4250 mmGlass, k = 0.96150 mmroom 20 °Coutside -9 °CQ̇

A wall of 250 mm concrete and 150 mm glass separates a room at 20 °C from outside air at -9 °C. The convection coefficients are 10 W/(m²·K) inside and 30 W/(m²·K) outside, and the wall area is 8 m². Find the overall heat transfer coefficient U of the wall.

L1 = 250 mm, k1 = 1.4 W/(m·K)L2 = 150 mm, k2 = 0.96 W/(m·K)A = 8 m²hi = 10 W/(m²·K)ho = 30 W/(m²·K)Troom = 20 °CTout = -9 °C
U = W/(m²·K)
21.Pipe friction & head lossMedium
Q = 20 L/sD = 200 mmL = 1000 mf = 0.018

Water flows at 20 L/s through a pipe 1000 m long with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.018 and g = 9.81 m/s². Find the friction head loss hf.

Q = 20 L/sL = 1000 mD = 200 mmf = 0.018g = 9.81 m/s²
hf = m
22.Pipe friction & head lossHard
K = 0.2free outletH = ?L = 100 m, D = 300 mm, f = 0.022× bend (K = 0.3)

A pipe 100 m long with an inside diameter of 300 mm (Darcy friction factor f = 0.02) 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 = 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 120 L/s?

Q = 120 L/sL = 100 mD = 300 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 0.2
H = m
23.Pumps & pump powerMedium
PQ = 150 L/sH = 60 m

In a test, a pump delivers 150 L/s of water (ρ = 1000 kg/m³) against a head of 60 m while its shaft takes 103.9 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 150 L/sH = 60 mPshaft = 103.9 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
PQ = 75 L/sΔz = 9 mL = 500 m, D = 200 mm, f = 0.015, ΣK = 6

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 9 m higher. The pipe is 500 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 = 6 (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 = 9 mL = 500 mD = 200 mmf = 0.015ΣK = 6η = 80%
Pshaft = kW

3Solutions

1.Mass balance

Answer: ṁ2 = 5000 kg/h

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

Balances

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

Solve for ṁ2

ṁ2 = ṁ1(x1 − x3)/(x3 − x2) = 1000·(40 − 15)/(15 − 10) = 5000 kg/h

Answer

ṁ2 = 5000 kg/h
2.Mass balance

Answer: W = 3326 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 = 4700·19/65 = 1374 kg/h

Total balance

W = F − P = 4700 − 1374 = 3326 kg/h

Answer

W = 3326 kg/h
3.Energy balance

Answer: tout = 41.4 °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) = 10 + 262.5/(2·4.18) = 41.4 °C

Answer

tout = 41.4 °C
4.Energy balance

Answer: ṁc = 0.5545 kg/s

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

Heat released

Qh = 1.5·2.44·(120 − 90) = 109.8 kW

Heat that reaches the water

Qc = (1 − 0.05)·109.8 = 104.3 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 104.3/(4.18·45) = 0.5545 kg/s

Answer

ṁc = 0.5545 kg/s
5.Ideal gas law

Answer: P = 92.62 kPa

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

Moles

n = m/M = 80/39.95 = 2.003 mol
T = 5 + 273.15 = 278.1 K

Pressure

P = nRT/V = 2.003·8.314·278.1/0.05 = 92.62 kPa

Answer

P = 92.62 kPa
6.Ideal gas law

Answer: ρ = 0.8957 kg/m³

Ideal gas density: ρ = PM/(RT).

Rearrange the gas law

PV = (m/M)RT → ρ = m/V = PM/(RT)
T = 130 + 273.15 = 403.1 K

Density

ρ = 750·4.003/(8.314·403.1) = 0.8957 kg/m³

Answer

ρ = 0.8957 kg/m³
7.Stoichiometry

Answer: m = 33.16 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(Mg) = 20/24.31 = 0.8227 mol
n(O2) = 64/32 = 2 mol

Limiting reactant

0.8227/2 = 0.4114, 2/1 = 2 → Mg

Mass of product

n(MgO) = 0.4114·2 = 0.8227 mol
m = 0.8227·40.3 = 33.16 g

Answer

m = 33.16 g
8.Stoichiometry

Answer: Y = 77.97 %

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(C6H12O6) = 24/180.16 = 0.1332 mol
m = 0.1332·2/1·46.07 = 12.27 g

Percent yield

Y = 9.57/12.27·100 = 77.97%

Answer

Y = 77.97%
9.Chemical equilibrium

Answer: [HI] = 0.24 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/(0.2 − x)²

Take the square root

3 = 2x/(0.2 − x) → x = 0.2·3/(2 + 3) = 0.12 mol/L

Equilibrium concentration

[HI] = 2x = 0.24 mol/L

Answer

[HI] = 0.24 mol/L
10.Chemical equilibrium

Answer: [Cl2] = 0.08956 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

0.05 = x²/(0.25 − x) → x² + 0.05·x − 0.0125 = 0

Solve the quadratic

x = (−0.05 + √(0.05² + 4·0.0125))/2 = 0.08956 mol/L

Equilibrium concentration

[Cl₂] = x = 0.08956 mol/L

Answer

[Cl2] = 0.08956 mol/L
11.Calorimetry & enthalpy

Answer: Tf = 23.84 °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

250·0.388·(90 − Tf) = 400·4.18·(Tf − 20)

Solve for the final temperature

Tf = (97·90 + 1672·20)/(97 + 1672) = 23.84 °C

Answer

Tf = 23.84 °C
12.Calorimetry & enthalpy

Answer: ΔH° = −2802 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

Answer

ΔH° = −2802 kJ

Negative: the reaction gives off heat (exothermic).

13.Reaction kinetics

Answer: t½ = 5 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).

Second-order half-life

t½ = 1/(k·CA0) = 1/(0.4·0.5) = 5 min

Answer

t½ = 5 min

Each later half-life is twice as long, because C₀ has halved.

14.Reaction kinetics

Answer: T2 = 51.73 °C

Reaction rates: for a first-order reaction −dC/dt = kC, so C = C₀·e−kt and the half-life ln 2/k does not depend on concentration. For a second-order reaction 1/C = 1/C₀ + kt. The rate constant rises with temperature following Arrhenius: k = A·e−Ea/(RT).

Absolute temperature

T1 = 313.1 K

Solve Arrhenius for T₂

1/T2 = 1/313.1 − 8.314·ln(2)/50000 = 3.193 × 10⁻³ − 1.153 × 10⁻⁴ = 3.078 × 10⁻³ K⁻¹
T2 = 324.9 K = 51.73 °C

Answer

T2 = 51.73 °C
15.Reactor sizing (CSTR & PFR)

Answer: VCSTR/VPFR = 2.987

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) = 0.85/0.15 = 5.667
PFR: k·τ = ln(1/(1 − X)) = ln(6.667) = 1.897

Ratio of volumes

VCSTR/VPFR = 5.667/1.897 = 2.987

Answer

VCSTR/VPFR = 2.987

The gap grows quickly at high conversion.

16.Reactor sizing (CSTR & PFR)

Answer: X = 31.27 %

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 = 200/80 = 2.5 min, kτ = 0.15·2.5 = 0.375

Conversion

X = 1 − e−kτ = 1 − e−0.375 = 31.27%

Answer

X = 31.27%
17.Heat exchangers (LMTD)

Answer: A = 15.55 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 (counter-flow)

In counter-flow the hot inlet faces the cold outlet, and the hot outlet faces the cold inlet.

ΔT₁ = Th,in − Tc,out = 145 − 60 = 85 K
ΔT₂ = Th,out − Tc,in = 55 − 30 = 25 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (85 − 25)/ln(85/25) = 49.03 K

Area

A = Q̇/(U·F·ΔTlm,cf) = 610000/(1000·0.8·49.03) = 15.55 m²

Answer

A = 15.55 m²
18.Heat exchangers (LMTD)

Answer: A = 0.9345 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) = 1·2.1·20 = 42 kW
Tc,out = 10 + 42/(1·4.18) = 20.05 °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 = 115 − 20.05 = 94.95 K
ΔT₂ = Th,out − Tc,in = 95 − 10 = 85 K

Log-mean temperature difference

ΔTlm = (ΔT₁ − ΔT₂)/ln(ΔT₁/ΔT₂) = (94.95 − 85)/ln(94.95/85) = 89.88 K

Area

A = Q̇/(U·ΔTlm) = 42000/(500·89.88) = 0.9345 m²

Answer

A = 0.9345 m²
19.Heat conduction

Answer: Q̇ = 532.9 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.

Layer resistances

R1 = L1/(k1A) = (50/1000)/(0.17·10) = 0.02941 K/W
R2 = L2/(k2A) = (150/1000)/(0.96·10) = 0.01563 K/W

Heat flow

Q̇ = (T1 − T3)/(R1 + R2) = 24/0.04504 = 532.9 W

Answer

Q̇ = 532.9 W
20.Heat conduction

Answer: U = 2.136 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/(10·8) = 0.0125 K/W
R1 = L1/(k1A) = (250/1000)/(1.4·8) = 0.02232 K/W
R2 = L2/(k2A) = (150/1000)/(0.96·8) = 0.01953 K/W
Ro = 1/(hoA) = 1/(30·8) = 0.004167 K/W
ΣR = 0.05852 K/W

Overall coefficient

U = 1/(A·ΣR) = 1/(8·0.05852) = 2.136 W/(m²·K)

Answer

U = 2.136 W/(m²·K)
21.Pipe friction & head loss

Answer: hf = 1.859 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·0.2²/4 = 0.03142 m²
V = Q/A = 0.02/0.03142 = 0.6366 m/s

Velocity head

V²/(2g) = 0.6366²/(2·9.81) = 0.02066 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.018·(1000/0.2)·0.6366²/(2·9.81) = 1.859 m

Answer

hf = 1.859 m
22.Pipe friction & head loss

Answer: H = 1.317 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 = 0.12/0.07069 = 1.698 m/s
V²/(2g) = 0.1469 m

Loss coefficients

f·L/D = 0.02·100/0.3 = 6.667
ΣK = 0.5 + 2·0.3 + 0.2 = 1.3

Energy equation

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

H = (1 + 6.667 + 1.3)·0.1469 = 1.317 m

Answer

H = 1.317 m
23.Pumps & pump power

Answer: η = 84.98 %

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 = 1000·9.81·0.15·60 = 88.29 kW

Efficiency

η = Ph/Pshaft = 88.29/103.9 = 84.98%

Answer

η = 84.98%
24.Pumps & pump power

Answer: Pshaft = 19.9 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) = (37.5 + 6)·0.2905 = 12.64 m

Pump head

H = Δz + hL = 9 + 12.64 = 21.64 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.075·21.64/0.8 = 19.9 kW

Answer

Pshaft = 19.9 kW

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