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
230 g of O₂P = 250 kPaT = 10 °CV = ?

What volume V does 230 g of O₂ occupy at 250 kPa and 10 °C? Treat it as an ideal gas.

m = 230 gM = 32 g/molP = 250 kPaT = 10 °CR = 8.314 J/(mol·K)
V = L
2.Ideal gas lawHard
State 1State 2

A fixed amount of Ar goes from 100 kPa, 5 L, 25 °C to 400 kPa and 150 °C. Find the new volume V2.

P1 = 100 kPaV1 = 5 LT1 = 25 °CP2 = 400 kPaT2 = 150 °C
V2 = L
3.Energy balanceMedium
hot sidecold sideglycol mix · 130 °C70 °Cwater · 15 °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 kg/scp,h = 3.6 kJ/(kg·K)Th: 130 → 70 °Cṁc = 1.5 kg/scp,c = 4.18 kJ/(kg·K)tin = 15 °C
tout = °C
4.Energy balanceHard
hot sidecold sidelight oil · 130 °C80 °Cwater · 15 °C55 °C · ṁ = ?10% lost

Hot light oil heats water in an exchanger that loses 10% of the heat released by the hot stream to the surroundings. Find the water flow rate ṁc needed.

ṁh = 0.5 kg/scp,h = 2.1 kJ/(kg·K)Th: 130 → 80 °Ct: 15 → 55 °Ccp,c = 4.18 kJ/(kg·K)loss = 10 %
ṁc = kg/s
5.Heat engines & refrigeratorsMedium
TH​ = 275 °CTL​ = 25 °CEQH​ = 4800 kJQL​W = ?

A heat engine works between a hot reservoir at 275 °C and a cold reservoir at 25 °C. It takes in 4800 kJ of heat. Find the most work Wmax it could possibly produce.

TH = 275 °CTL = 25 °CQH = 4800 kJ
Wmax = kJ
6.Heat engines & refrigeratorsHard
TH​ = 850 °CTL​ = 30 °CEQH​ = 2100 kJQL​ = 1323 kJW = 777 kJ

A heat engine takes in 2100 kJ of heat from a reservoir at 850 °C, produces 777 kJ of work and rejects the rest to a reservoir at 30 °C, per cycle. Find the total entropy generated Sgen per cycle.

TH = 850 °CTL = 30 °CQH = 2100 kJW = 777 kJ
Sgen = kJ/K
7.Gas power cyclesMedium
vP1234qin​qout​

An ideal Diesel cycle has a compression ratio r = 14 and a cutoff ratio rc = v₃/v₂ = 3. 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 = 3T1 = 305 Kk = 1.4
T3 = K
8.Gas power cyclesHard
vP1234qin​qout​

An ideal Brayton cycle operates with a compressor pressure ratio of 10. 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 = 10k = 1.4
η = %

3Solutions

1.Ideal gas law

Answer: V = 67.68 L

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

Moles

n = 230/32 = 7.188 mol
T = 10 + 273.15 = 283.1 K

Volume

V = nRT/P = 7.188·8.314·283.1/250 = 67.68 L

Answer

V = 67.68 L
2.Ideal gas law

Answer: V2 = 1.774 L

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

Absolute temperatures

T1 = 298.1 K, T2 = 423.1 K

Combined gas law

V2 = V1·(P1/P2)·(T2/T1) = 5·(100/400)·(423.1/298.1) = 1.774 L

Answer

V2 = 1.774 L
3.Energy balance

Answer: tout = 83.9 °C

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

Heat released by the hot stream

Q = 2·3.6·(130 − 70) = 432 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 15 + 432/(1.5·4.18) = 83.9 °C

Answer

tout = 83.9 °C
4.Energy balance

Answer: ṁc = 0.2826 kg/s

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

Heat released

Qh = 0.5·2.1·(130 − 80) = 52.5 kW

Heat that reaches the water

Qc = (1 − 0.1)·52.5 = 47.25 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 47.25/(4.18·40) = 0.2826 kg/s

Answer

ṁc = 0.2826 kg/s
5.Heat engines & refrigerators

Answer: Wmax = 2189 kJ

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 = 275 + 273.15 = 548.1 K
TL = 25 + 273.15 = 298.1 K

Carnot efficiency

ηmax = 1 − TL/TH = 1 − 298.1/548.1 = 45.61 %

Maximum work

Wmax = ηmax·QH = 0.4561·4800 = 2189 kJ

Answer

Wmax = 2189 kJ
6.Heat engines & refrigerators

Answer: Sgen = 2.494 kJ/K

Entropy generation: over a full cycle the working fluid has no net entropy change. The hot reservoir loses QH/TH and the cold reservoir gains QL/TL. Their sum is the entropy generated, which is zero for a reversible cycle and positive for every real one.

Heat rejected

QL = QH − W = 2100 − 777 = 1323 kJ

Absolute temperatures

TH = 850 + 273.15 = 1123 K
TL = 30 + 273.15 = 303.1 K

Entropy changes of the reservoirs

ΔSH = −2100/1123 = −1.87 kJ/K
ΔSL = 1323/303.1 = 4.364 kJ/K
Sgen = 4.364 − 1.87 = 2.494 kJ/K

Answer

Sgen = 2.494 kJ/K

Sgen > 0, so the engine is possible but irreversible.

7.Gas power cycles

Answer: T3 = 2629 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 = 3·876.5 = 2629 K

Answer

T3 = 2629 K
8.Gas power cycles

Answer: η = 48.21 %

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 − 1/100.2857 = 1 − 1/1.931 = 48.21%

Answer

η = 48.21%

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