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
80 g of CH₄P = 200 kPaT = 90 °CV = ?

What volume V does 80 g of CH₄ occupy at 200 kPa and 90 °C? Treat it as an ideal gas.

m = 80 gM = 16.04 g/molP = 200 kPaT = 90 °CR = 8.314 J/(mol·K)
V = L
2.Ideal gas lawHard
State 1State 2

A fixed amount of O₂ goes from 400 kPa, 2 L, 40 °C to 150 kPa and 130 °C. Find the new volume V2.

P1 = 400 kPaV1 = 2 LT1 = 40 °CP2 = 150 kPaT2 = 130 °C
V2 = L
3.Energy balanceMedium
hot sidecold sidelight oil · 150 °C80 °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 = 0.5 kg/scp,h = 2.1 kJ/(kg·K)Th: 150 → 80 °Cṁc = 0.5 kg/scp,c = 4.18 kJ/(kg·K)tin = 10 °C
tout = °C
4.Energy balanceHard
hot sidecold sideglycol mix · 150 °C80 °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 = 2.5 kg/scp,h = 3.6 kJ/(kg·K)Th: 150 → 80 °Ct: 20 → 80 °Ccp,c = 4.18 kJ/(kg·K)loss = 15 %
ṁc = kg/s
5.Heat engines & refrigeratorsMedium
TH​ = 700 °CTL​ = ?EQH​ = 4900 kJQL​ = 1627 kJW

A reversible (Carnot) heat engine takes in 4900 kJ of heat from a reservoir at 700 °C and rejects 1627 kJ per cycle. Find the temperature TL of the cold reservoir in °C.

TH = 700 °CQH = 4900 kJQL = 1627 kJ
TL = °C
6.Heat engines & refrigeratorsHard
TH​ = 650 °CT0​ = 20 °CTL​ = -25 °CERWQ̇H​ = 80 kWQ̇L​ = ?

A Carnot heat engine receives 80 kW of heat from a source at 650 °C and rejects heat to the surroundings at 20 °C. All of its work drives a Carnot refrigerator that removes heat from a freezer at -25 °C and also rejects heat to the surroundings at 20 °C. Find the rate Q̇L at which heat is removed from the freezer.

TH = 650 °CT0 = 20 °CTL = -25 °CQ̇H = 80 kW
Q̇L = kW
7.Gas power cyclesMedium
vP1234qin​qout​

An ideal Diesel cycle has a compression ratio r = 19 and a cutoff ratio rc = v₃/v₂ = 1.8. At the start of compression the air is at 320 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 = 1.8T1 = 320 Kk = 1.4cp = 1.005 kJ/(kg·K)
qin = kJ/kg
8.Gas power cyclesHard
vP1234qin​qout​

A gas-turbine plant runs on a Brayton cycle with a compressor pressure ratio of 6. Air enters the compressor at 300 K and the turbine at 1100 K. The compressor has an isentropic efficiency of 80% and the turbine 90%. 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 net work output wnet per kilogram of air, in kJ/kg.

rp = 6T1 = 300 KT3 = 1100 Kηc = 80%ηt = 90%k = 1.4cp = 1.005 kJ/(kg·K)
wnet = kJ/kg

3Solutions

1.Ideal gas law

Answer: V = 75.29 L

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

Moles

n = 80/16.04 = 4.988 mol
T = 90 + 273.15 = 363.1 K

Volume

V = nRT/P = 4.988·8.314·363.1/200 = 75.29 L

Answer

V = 75.29 L
2.Ideal gas law

Answer: V2 = 6.866 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·(400/150)·(403.1/313.1) = 6.866 L

Answer

V2 = 6.866 L
3.Energy balance

Answer: tout = 45.17 °C

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

Heat released by the hot stream

Q = 0.5·2.1·(150 − 80) = 73.5 kW

Heat picked up by the water

tout = tin + Q/(ṁccp,c) = 10 + 73.5/(0.5·4.18) = 45.17 °C

Answer

tout = 45.17 °C
4.Energy balance

Answer: ṁc = 2.135 kg/s

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

Heat released

Qh = 2.5·3.6·(150 − 80) = 630 kW

Heat that reaches the water

Qc = (1 − 0.15)·630 = 535.5 kW

Water flow rate

ṁc = Qc/(cp,c·Δt) = 535.5/(4.18·60) = 2.135 kg/s

Answer

ṁc = 2.135 kg/s
5.Heat engines & refrigerators

Answer: TL = 49.98 °C

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 temperature of the source

TH = 700 + 273.15 = 973.1 K

Reversible heat ratio

TL = TH·QL/QH = 973.1·1627/4900 = 323.1 K = 49.98 °C

Answer

TL = 49.98 °C
6.Heat engines & refrigerators

Answer: Q̇L = 301.1 kW

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 = 650 + 273.15 = 923.1 K
T0 = 20 + 273.15 = 293.1 K
TL = -25 + 273.15 = 248.1 K

Engine work

η = 1 − 293.1/923.1 = 0.6824
Ẇ = 0.6824·80 = 54.6 kW

Heat removed by the refrigerator

COPR = 248.1/(293.1 − 248.1) = 5.514
Q̇L = 5.514·54.6 = 301.1 kW

Answer

Q̇L = 301.1 kW
7.Gas power cycles

Answer: qin = 835.4 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 = 320·190.4 = 1039 K
T3 = 1.8·1039 = 1870 K

Heat added at constant pressure

qin = 1.005·(1870 − 1039) = 835.4 kJ/kg

Answer

qin = 835.4 kJ/kg
8.Gas power cycles

Answer: wnet = 146.7 kJ/kg

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.

Isentropic temperatures

T2s = 300·60.2857 = 500.6 K
T4s = 1100/60.2857 = 659.3 K

Compressor and turbine work

wc = 1.005·(500.6 − 300)/0.8 = 251.9 kJ/kg
wt = 0.9·1.005·(1100 − 659.3) = 398.6 kJ/kg

Net work

wnet = 398.6 − 251.9 = 146.7 kJ/kg

Answer

wnet = 146.7 kJ/kg

Back-work ratio: wc/wt = 63.2%.

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