Thermodynamics 1: cram pack

Formula sheets, the key method steps for every topic and 8 practice problems, with full solutions at the back.

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1Formulas and methods

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

Energy balance

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

Heat engines & refrigerators

Efficiency
η = W/QH = 1 − QC/QH
Carnot efficiency
ηC = 1 − TC/TH (kelvin)
Refrigerator COP
COPR = QC/W
Heat pump COP
COPHP = QH/W = COPR + 1
Energy balance
QH = W + QC

Gas power cycles

Isentropic, volume ratio
T2/T1 = rk−1
Isentropic, pressure ratio
T2/T1 = rp(k−1)/k
Otto efficiency
η = 1 − 1/rk−1
Diesel efficiency
η = 1 − (1/rk−1)·(rck − 1)/(k(rc − 1))
Brayton efficiency
η = 1 − 1/rp(k−1)/k
Heat added
Otto: cv(T3 − T2) Diesel, Brayton: cp(T3 − T2)
Brayton net work
w = cp[(T3 − T4) − (T2 − T1)]
Isentropic efficiencies
wc = wc,s/ηc, wt = ηt·wt,s
Cold air
k = 1.4, cp = 1.005, cv = 0.718 kJ/(kg·K)

2Practice problems

1.Ideal gas lawMedium
330 g of HeV = 20 LT = 80 °CP = ?

A tank of 20 L contains 330 g of He at 80 °C. Treat it as an ideal gas and find the pressure P.

m = 330 gM = 4.003 g/molV = 20 LT = 80 °CR = 8.314 J/(mol·K)
P = kPa
2.Ideal gas lawHard
CH₄, M = 16.04 g/molP = 550 kPaT = 170 °Cρ = ?

Find the density ρ of CH₄ at 550 kPa and 170 °C, treating it as an ideal gas.

M = 16.04 g/molP = 550 kPaT = 170 °CR = 8.314 J/(mol·K)
ρ = kg/m³
3.Energy balanceMedium
hot sidecold sideethanol · 150 °C120 °Cwater · 15 °Ct = ? °C

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

ṁh = 1.5 kg/scp,h = 2.44 kJ/(kg·K)Th: 150 → 120 °Cṁc = 1 kg/scp,c = 4.18 kJ/(kg·K)tin = 15 °C
tout = °C
4.Energy balanceHard
hot sidecold sidelight oil · 160 °C80 °Cwater · 10 °C45 °C · ṁ = ?5% lost

Hot light oil 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 = 2.5 kg/scp,h = 2.1 kJ/(kg·K)Th: 160 → 80 °Ct: 10 → 45 °Ccp,c = 4.18 kJ/(kg·K)loss = 5 %
ṁc = kg/s
5.Heat engines & refrigeratorsMedium
TH​ = 425 °CTL​ = 15 °CEQH​QL​W

A heat engine works between a hot reservoir at 425 °C and a cold reservoir at 15 °C. Find the highest possible thermal efficiency ηmax.

TH = 425 °CTL = 15 °C
ηmax = %
6.Heat engines & refrigeratorsHard
TH​ = 20 °CTL​ = -5 °CHPQ̇H​ = 6 kWQ̇L​Ẇ

A heat pump keeps a house at 20 °C while it is -5 °C outside, delivering 6 kW of heat to the house. Find the highest possible coefficient of performance COPmax.

TH = 20 °CTL = -5 °CQ̇H = 6 kW
COPmax =
7.Gas power cyclesMedium
vP1234qin​qout​

An ideal Diesel cycle has a compression ratio r = 14 and a cutoff ratio rc = v₃/v₂ = 2.5. At the start of compression the air is at 305 K. Use the cold-air-standard assumptions: air is an ideal gas with constant specific heats, k = 1.4, cp = 1.005 kJ/(kg·K) and cv = 0.718 kJ/(kg·K). Find the temperature T3 at the end of heat addition, in K.

r = 14rc = 2.5T1 = 305 Kk = 1.4
T3 = K
8.Gas power cyclesHard
vP1234qin​qout​

An ideal Brayton cycle operates with a compressor pressure ratio of 20. Use the cold-air-standard assumptions: air is an ideal gas with constant specific heats, k = 1.4, cp = 1.005 kJ/(kg·K) and cv = 0.718 kJ/(kg·K). Find its thermal efficiency η in percent.

rp = 20k = 1.4
η = %

3Solutions

1.Ideal gas law

Answer: P = 12102 kPa

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

Moles

n = m/M = 330/4.003 = 82.44 mol
T = 80 + 273.15 = 353.1 K

Pressure

P = nRT/V = 82.44·8.314·353.1/0.02 = 12102 kPa

Answer

P = 12102 kPa
2.Ideal gas law

Answer: ρ = 2.394 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 = 550·16.04/(8.314·443.1) = 2.394 kg/m³

Answer

ρ = 2.394 kg/m³
3.Energy balance

Answer: tout = 41.27 °C

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

Heat released by the hot stream

Q = 1.5·2.44·(150 − 120) = 109.8 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 15 + 109.8/(1·4.18) = 41.27 °C

Answer

tout = 41.27 °C
4.Energy balance

Answer: ṁc = 2.727 kg/s

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

Heat released

Qh = 2.5·2.1·(160 − 80) = 420 kW

Heat that reaches the water

Qc = (1 − 0.05)·420 = 399 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 399/(4.18·35) = 2.727 kg/s

Answer

ṁc = 2.727 kg/s
5.Heat engines & refrigerators

Answer: ηmax = 58.73 %

Second-law limits: no cycle working between reservoirs at absolute temperatures TH and TL can beat the reversible (Carnot) cycle: ηmax = 1 − TL/TH, COPR,max = TL/(TH − TL) and COPHP,max = TH/(TH − TL). Energy is always conserved: QH = W + QL.

Absolute temperatures

TH = 425 + 273.15 = 698.1 K
TL = 15 + 273.15 = 288.1 K

Carnot efficiency

ηmax = 1 − TL/TH = 1 − 288.1/698.1 = 58.73 %

Answer

ηmax = 58.73 %
6.Heat engines & refrigerators

Answer: COPmax = 11.73

Second-law limits: no cycle working between reservoirs at absolute temperatures TH and TL can beat the reversible (Carnot) cycle: ηmax = 1 − TL/TH, COPR,max = TL/(TH − TL) and COPHP,max = TH/(TH − TL). Energy is always conserved: QH = W + QL.

Absolute temperatures

TH = 20 + 273.15 = 293.1 K
TL = -5 + 273.15 = 268.1 K

Best possible COP

COPHP,max = TH/(TH − TL) = 293.1/(293.1 − 268.1) = 11.73

Answer

COPmax = 11.73
7.Gas power cycles

Answer: T3 = 2191 K

Diesel cycle (compression-ignition engine): 1→2 isentropic compression, 2→3 heat addition at constant pressure, 3→4 isentropic expansion, 4→1 heat rejection at constant volume. With compression ratio r = v₁/v₂ and cutoff ratio rc = v₃/v₂: T₂ = T₁·rk−1, T₃ = rc·T₂, qin = cp·(T₃ − T₂) and η = 1 − (1/rk−1)·(rck − 1)/(k·(rc − 1)).

End of compression

T2 = 305·140.4 = 876.5 K

Heat addition at constant pressure

T3 = rc·T2 = 2.5·876.5 = 2191 K

Answer

T3 = 2191 K
8.Gas power cycles

Answer: η = 57.51 %

Brayton cycle (gas turbine): 1→2 isentropic compression, 2→3 heat addition at constant pressure, 3→4 isentropic expansion in the turbine, 4→1 heat rejection at constant pressure. With pressure ratio rp = P₂/P₁: T₂ = T₁·rp(k−1)/k, T₄ = T₃/rp(k−1)/k and η = 1 − 1/rp(k−1)/k. Net work w = cp·[(T₃ − T₄) − (T₂ − T₁)]. With isentropic efficiencies, the compressor needs ws/ηc and the turbine gives ηt·ws.

Thermal efficiency

η = 1 − 1/200.2857 = 1 − 1/2.354 = 57.51%

Answer

η = 57.51%

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