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
340 g of N₂P = 600 kPaT = 40 °CV = ?

What volume V does 340 g of N₂ occupy at 600 kPa and 40 °C? Treat it as an ideal gas.

m = 340 gM = 28.01 g/molP = 600 kPaT = 40 °CR = 8.314 J/(mol·K)
V = L
2.Ideal gas lawHard
State 1State 2

A fixed amount of O₂ goes from 200 kPa, 2 L, 40 °C to 200 kPa and 130 °C. Find the new volume V2.

P1 = 200 kPaV1 = 2 LT1 = 40 °CP2 = 200 kPaT2 = 130 °C
V2 = L
3.Energy balanceMedium
hot sidecold sidelight oil · 160 °C90 °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: 160 → 90 °Cṁc = 1 kg/scp,c = 4.18 kJ/(kg·K)tin = 25 °C
tout = °C
4.Energy balanceHard
hot sidecold sideethanol · 180 °C120 °Cwater · 15 °C40 °C · ṁ = ?15% lost

Hot ethanol 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 = 2.44 kJ/(kg·K)Th: 180 → 120 °Ct: 15 → 40 °Ccp,c = 4.18 kJ/(kg·K)loss = 15 %
ṁc = kg/s
5.Heat engines & refrigeratorsMedium
TH​ = 775 °CTL​ = 25 °CEQH​QL​W

A heat engine works between a hot reservoir at 775 °C and a cold reservoir at 25 °C. Find the highest possible thermal efficiency ηmax.

TH = 775 °CTL = 25 °C
ηmax = %
6.Heat engines & refrigeratorsHard
TH​ = 35 °CTL​ = -18 °CRQ̇H​Q̇L​ = 4.5 kWẆ

A refrigerator keeps its cold space at -18 °C in a kitchen at 35 °C, removing heat from the cold space at 4.5 kW. Find the highest possible coefficient of performance COPmax.

TH = 35 °CTL = -18 °CQ̇L = 4.5 kW
COPmax =
7.Gas power cyclesMedium
vP1234qin​qout​

An ideal Diesel cycle has a compression ratio r = 19 and a cutoff ratio rc = v₃/v₂ = 2. At the start of compression the air is at 295 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 heat added qin per kilogram of air, in kJ/kg.

r = 19rc = 2T1 = 295 Kk = 1.4cp = 1.005 kJ/(kg·K)
qin = kJ/kg
8.Gas power cyclesHard
vP1234qin​qout​

An ideal Brayton cycle operates with a compressor pressure ratio of 14. 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 = 14k = 1.4
η = %

3Solutions

1.Ideal gas law

Answer: V = 52.67 L

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

Moles

n = 340/28.01 = 12.14 mol
T = 40 + 273.15 = 313.1 K

Volume

V = nRT/P = 12.14·8.314·313.1/600 = 52.67 L

Answer

V = 52.67 L
2.Ideal gas law

Answer: V2 = 2.575 L

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

Absolute temperatures

T1 = 313.1 K, T2 = 403.1 K

Combined gas law

V2 = V1·(P1/P2)·(T2/T1) = 2·(200/200)·(403.1/313.1) = 2.575 L

Answer

V2 = 2.575 L
3.Energy balance

Answer: tout = 130.5 °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·(160 − 90) = 441 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 25 + 441/(1·4.18) = 130.5 °C

Answer

tout = 130.5 °C
4.Energy balance

Answer: ṁc = 1.191 kg/s

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

Heat released

Qh = 1·2.44·(180 − 120) = 146.4 kW

Heat that reaches the water

Qc = (1 − 0.15)·146.4 = 124.4 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 124.4/(4.18·25) = 1.191 kg/s

Answer

ṁc = 1.191 kg/s
5.Heat engines & refrigerators

Answer: ηmax = 71.55 %

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 = 775 + 273.15 = 1048 K
TL = 25 + 273.15 = 298.1 K

Carnot efficiency

ηmax = 1 − TL/TH = 1 − 298.1/1048 = 71.55 %

Answer

ηmax = 71.55 %
6.Heat engines & refrigerators

Answer: COPmax = 4.814

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 = 35 + 273.15 = 308.1 K
TL = -18 + 273.15 = 255.1 K

Best possible COP

COPR,max = TL/(TH − TL) = 255.1/(308.1 − 255.1) = 4.814

Answer

COPmax = 4.814
7.Gas power cycles

Answer: qin = 962.7 kJ/kg

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)).

Temperatures

T2 = 295·190.4 = 957.9 K
T3 = 2·957.9 = 1916 K

Heat added at constant pressure

qin = 1.005·(1916 − 957.9) = 962.7 kJ/kg

Answer

qin = 962.7 kJ/kg
8.Gas power cycles

Answer: η = 52.95 %

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 − 1/140.2857 = 1 − 1/2.126 = 52.95%

Answer

η = 52.95%

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