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·c_p·ΔT
Latent heat: Q = ṁ·h_fg
Mixing: Σṁc_pT_in = Σṁc_pT_out
Water: c_p ≈ 4.18 kJ/(kg·K)

Heat engines & refrigerators

Efficiency: η = W/Q_H = 1 − Q_C/Q_H
Carnot efficiency: η_C = 1 − T_C/T_H (kelvin)
Refrigerator COP: COP_R = Q_C/W
Heat pump COP: COP_HP = Q_H/W = COP_R + 1
Energy balance: Q_H = W + Q_C

Gas power cycles

Isentropic, volume ratio: T₂/T₁ = r^k−1
Isentropic, pressure ratio: T₂/T₁ = r_p^(k−1)/k
Otto efficiency: η = 1 − 1/r^k−1
Diesel efficiency: η = 1 − (1/r^k−1)·(r_c^k − 1)/(k(r_c − 1))
Brayton efficiency: η = 1 − 1/r_p^(k−1)/k
Heat added: Otto: c_v(T₃ − T₂) Diesel, Brayton: c_p(T₃ − T₂)
Brayton net work: w = c_p[(T₃ − T₄) − (T₂ − T₁)]
Isentropic efficiencies: w_c = w_c,s/η_c, w_t = η_t·w_t,s
Cold air: k = 1.4, c_p = 1.005, c_v = 0.718 kJ/(kg·K)

2Practice problems

1.Ideal gas lawMedium

What volume V does 230 g of CO₂ occupy at 550 kPa and 70 °C? Treat it as an ideal gas.

m = 230 gM = 44.01 g/molP = 550 kPaT = 70 °CR = 8.314 J/(mol·K)

V = L

2.Ideal gas lawHard

Find the density ρ of O₂ at 250 kPa and 50 °C, treating it as an ideal gas.

M = 32 g/molP = 250 kPaT = 50 °CR = 8.314 J/(mol·K)

ρ = kg/m³

3.Energy balanceMedium

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

ṁ_h = 3 kg/sc_p,h = 2.44 kJ/(kg·K)T_h: 170 → 130 °Cṁ_c = 3 kg/sc_p,c = 4.18 kJ/(kg·K)t_in = 20 °C

t_out = °C

4.Energy balanceHard

Hot light oil heats water in an exchanger that loses 15% of the heat released by the hot stream to the surroundings. Find the water flow rate ṁ_c needed.

ṁ_h = 1 kg/sc_p,h = 2.1 kJ/(kg·K)T_h: 120 → 70 °Ct: 25 → 50 °Cc_p,c = 4.18 kJ/(kg·K)loss = 15 %

ṁ_c = kg/s

5.Heat engines & refrigeratorsMedium

A heat engine works between a hot reservoir at 750 °C and a cold reservoir at 35 °C. It takes in 3500 kJ of heat. Find the most work W_max it could possibly produce.

T_H = 750 °CT_L = 35 °CQ_H = 3500 kJ

W_max = kJ

6.Heat engines & refrigeratorsHard

A heat pump delivers 15 kW of heat to a heating system at 55 °C, taking heat from a source at 0 °C. Its actual COP is 50% of the Carnot COP between these temperatures. Find the electrical power Ẇ it uses.

T_H = 55 °CT_L = 0 °Cη_II = 50%Q̇_H = 15 kW

Ẇ = kW

7.Gas power cyclesMedium

An ideal Diesel cycle has a compression ratio r = 17 and a cutoff ratio r_c = v₃/v₂ = 2. At the start of compression the air is at 310 K. Use the cold-air-standard assumptions: air is an ideal gas with constant specific heats, k = 1.4, c_p = 1.005 kJ/(kg·K) and c_v = 0.718 kJ/(kg·K). Find the temperature T₃ at the end of heat addition, in K.

r = 17r_c = 2T₁ = 310 Kk = 1.4

T₃ = K

8.Gas power cyclesHard

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, c_p = 1.005 kJ/(kg·K) and c_v = 0.718 kJ/(kg·K). Find its thermal efficiency η in percent.

r_p = 16k = 1.4

η = %

3Solutions

1.Ideal gas law

Answer: V = 27.11 L

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

Moles

n = 230/44.01 = 5.226 mol

T = 70 + 273.15 = 343.1 K

Volume

V = nRT/P = 5.226·8.314·343.1/550 = 27.11 L

Answer

V = 27.11 L

2.Ideal gas law

Answer: ρ = 2.978 kg/m³

Ideal gas density: ρ = PM/(RT).

Rearrange the gas law

PV = (m/M)RT → ρ = m/V = PM/(RT)

T = 50 + 273.15 = 323.1 K

Density

ρ = 250·32/(8.314·323.1) = 2.978 kg/m³

Answer

ρ = 2.978 kg/m³

3.Energy balance

Answer: t_out = 43.35 °C

Exchanger energy balance: with no losses, ṁ_hc_p,h(T_h,in − T_h,out) = ṁ_cc_p,c(t_out − t_in).

Heat released by the hot stream

Q = 3·2.44·(170 − 130) = 292.8 kW

Heat picked up by the water

t_out = t_in + Q/(ṁ_cc_p,c) = 20 + 292.8/(3·4.18) = 43.35 °C

Answer

t_out = 43.35 °C

4.Energy balance

Answer: ṁ_c = 0.8541 kg/s

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

Heat released

Q_h = 1·2.1·(120 − 70) = 105 kW

Heat that reaches the water

Q_c = (1 − 0.15)·105 = 89.25 kW

Water flow rate

ṁ_c = Q_c/(c_p,c·Δt) = 89.25/(4.18·25) = 0.8541 kg/s

Answer

ṁ_c = 0.8541 kg/s

5.Heat engines & refrigerators

Answer: W_max = 2446 kJ

Second-law limits: no cycle working between reservoirs at absolute temperatures T_H and T_L can beat the reversible (Carnot) cycle: η_max = 1 − T_L/T_H, COP_R,max = T_L/(T_H − T_L) and COP_HP,max = T_H/(T_H − T_L). Energy is always conserved: Q_H = W + Q_L.

Absolute temperatures

T_H = 750 + 273.15 = 1023 K

T_L = 35 + 273.15 = 308.1 K

Carnot efficiency

η_max = 1 − T_L/T_H = 1 − 308.1/1023 = 69.88 %

Maximum work

W_max = η_max·Q_H = 0.6988·3500 = 2446 kJ

Answer

W_max = 2446 kJ

6.Heat engines & refrigerators

Answer: Ẇ = 5.028 kW

Absolute temperatures

T_H = 55 + 273.15 = 328.1 K

T_L = 0 + 273.15 = 273.1 K

Carnot and actual COP

COP_max = 328.1/(328.1 − 273.1) = 5.966

COP = 0.5·5.966 = 2.983

Power input

Ẇ = Q̇_H/COP = 15/2.983 = 5.028 kW

Answer

Ẇ = 5.028 kW

7.Gas power cycles

Answer: T₃ = 1926 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 r_c = v₃/v₂: T₂ = T₁·r^k−1, T₃ = r_c·T₂, q_in = c_p·(T₃ − T₂) and η = 1 − (1/r^k−1)·(r_c^k − 1)/(k·(r_c − 1)).

End of compression

T₂ = 310·17^0.4 = 962.8 K

Heat addition at constant pressure

T₃ = r_c·T₂ = 2·962.8 = 1926 K

Answer

T₃ = 1926 K

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 r_p = P₂/P₁: T₂ = T₁·r_p^(k−1)/k, T₄ = T₃/r_p^(k−1)/k and η = 1 − 1/r_p^(k−1)/k. Net work w = c_p·[(T₃ − T₄) − (T₂ − T₁)]. With isentropic efficiencies, the compressor needs w_s/η_c and the turbine gives η_t·w_s.

Thermal efficiency

η = 1 − 1/16^0.2857 = 1 − 1/2.208 = 54.71%

Answer

η = 54.71%

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