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
300 g of HeP = 600 kPaT = 55 °CV = ?

What volume V does 300 g of He occupy at 600 kPa and 55 °C? Treat it as an ideal gas.

m = 300 gM = 4.003 g/molP = 600 kPaT = 55 °CR = 8.314 J/(mol·K)
V = L
2.Ideal gas lawHard
O₂, M = 32 g/molP = 500 kPaT = 140 °Cρ = ?

Find the density ρ of O₂ at 500 kPa and 140 °C, treating it as an ideal gas.

M = 32 g/molP = 500 kPaT = 140 °CR = 8.314 J/(mol·K)
ρ = kg/m³
3.Energy balanceMedium
hot sidecold sidelight oil · 120 °C80 °Cwater · 25 °Ct = ? °C

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

ṁh = 3 kg/scp,h = 2.1 kJ/(kg·K)Th: 120 → 80 °Cṁc = 1.5 kg/scp,c = 4.18 kJ/(kg·K)tin = 25 °C
tout = °C
4.Energy balanceHard
hot sidecold sideglycol mix · 150 °C110 °Cwater · 20 °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 = 1 kg/scp,h = 3.6 kJ/(kg·K)Th: 150 → 110 °Ct: 20 → 80 °Ccp,c = 4.18 kJ/(kg·K)loss = 15 %
ṁc = kg/s
5.Heat engines & refrigeratorsMedium
TH​ = 425 °CTL​ = 20 °CEQH​ = 3200 kJQL​W = ?

A heat engine works between a hot reservoir at 425 °C and a cold reservoir at 20 °C. It takes in 3200 kJ of heat. Find the most work Wmax it could possibly produce.

TH = 425 °CTL = 20 °CQH = 3200 kJ
Wmax = kJ
6.Heat engines & refrigeratorsHard
TH​ = 22 °CTL​ = -10 °CHPQ̇H​ = 8 kWQ̇L​Ẇ

A heat pump keeps a house at 22 °C while it is -10 °C outside, delivering 8 kW of heat to the house. Find the highest possible coefficient of performance COPmax.

TH = 22 °CTL = -10 °CQ̇H = 8 kW
COPmax =
7.Gas power cyclesMedium
vP1234qin​qout​

An ideal Diesel cycle has a compression ratio r = 17 and a cutoff ratio rc = v₃/v₂ = 1.5. 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.

r = 17rc = 1.5k = 1.4
η = %
8.Gas power cyclesHard
vP1234qin​qout​

An ideal Brayton cycle operates with a compressor pressure ratio of 16. 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 = 16k = 1.4
η = %

3Solutions

1.Ideal gas law

Answer: V = 340.8 L

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

Moles

n = 300/4.003 = 74.94 mol
T = 55 + 273.15 = 328.1 K

Volume

V = nRT/P = 74.94·8.314·328.1/600 = 340.8 L

Answer

V = 340.8 L
2.Ideal gas law

Answer: ρ = 4.658 kg/m³

Ideal gas density: ρ = PM/(RT).

Rearrange the gas law

PV = (m/M)RT → ρ = m/V = PM/(RT)
T = 140 + 273.15 = 413.1 K

Density

ρ = 500·32/(8.314·413.1) = 4.658 kg/m³

Answer

ρ = 4.658 kg/m³
3.Energy balance

Answer: tout = 65.19 °C

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

Heat released by the hot stream

Q = 3·2.1·(120 − 80) = 252 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 25 + 252/(1.5·4.18) = 65.19 °C

Answer

tout = 65.19 °C
4.Energy balance

Answer: ṁc = 0.488 kg/s

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

Heat released

Qh = 1·3.6·(150 − 110) = 144 kW

Heat that reaches the water

Qc = (1 − 0.15)·144 = 122.4 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 122.4/(4.18·60) = 0.488 kg/s

Answer

ṁc = 0.488 kg/s
5.Heat engines & refrigerators

Answer: Wmax = 1856 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 = 425 + 273.15 = 698.1 K
TL = 20 + 273.15 = 293.1 K

Carnot efficiency

ηmax = 1 − TL/TH = 1 − 293.1/698.1 = 58.01 %

Maximum work

Wmax = ηmax·QH = 0.5801·3200 = 1856 kJ

Answer

Wmax = 1856 kJ
6.Heat engines & refrigerators

Answer: COPmax = 9.223

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 = 22 + 273.15 = 295.1 K
TL = -10 + 273.15 = 263.1 K

Best possible COP

COPHP,max = TH/(TH − TL) = 295.1/(295.1 − 263.1) = 9.223

Answer

COPmax = 9.223
7.Gas power cycles

Answer: η = 64.85 %

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)).

Cutoff term

(1.51.4 − 1)/(1.4·(1.5 − 1)) = 1.092

Thermal efficiency

η = 1 − 0.322·1.092 = 64.85%

Answer

η = 64.85%
8.Gas power cycles

Answer: η = 54.71 %

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 − 1/160.2857 = 1 − 1/2.208 = 54.71%

Answer

η = 54.71%

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