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Diesel cycle with compression ratio 15:1

Short answer

Assuming 1675 kJ/kg heat added, T2=924.66 K and p2=4.431 MPa. Maximum temperature is T3=2591.3 K and maximum pressure is 4.431 MPa; cut-off ratio is 2.802. Net work is 948.6 kJ/kg, thermal efficiency is 56.64%, and mean effective pressure is 1131.5 kPa (11.31 bar).

In a diesel power plant engine is coupled with an alternator. The engine has compression ratio 15:1. The compression begins at 0.1MPa and 40°C. The heat added at the end of compression is 1675MJ/kg. Consider air constant, R = 287 kJ/kgK and Find: (i) The maximum temperature and pressure in the cycle (ii) The cut off ratio of the engine (iii) Net work done per kg of air (iv) Thermal efficiency of the engine (v) Mean effective pressure of the cycle.

Assumptions: the engine works on the air-standard Diesel cycle (isentropic compression 1–2, constant-pressure heat addition 2–3, isentropic expansion 3–4, constant-volume heat rejection 4–1). The heat added is taken as 1675 kJ/kg (1675 MJ/kg is clearly a misprint), R=0.287R = 0.287 kJ/kg K, cp=1.005c_p = 1.005, cv=0.718c_v = 0.718 kJ/kg K, γ=1.4\gamma = 1.4.

Data: r=15r = 15, p1=0.1p_1 = 0.1 MPa, T1=40+273=313T_1 = 40 + 273 = 313 K.

(i) Maximum temperature and pressure

Process 1–2 (isentropic compression):

T2=T1rγ−1=313×150.4=924.66 Kp2=p1rγ=0.1×151.4=4.431 MPa\begin{aligned} T_2 &= T_1 r^{\gamma-1} = 313 \times 15^{0.4} = 924.66\ \text{K} \\ p_2 &= p_1 r^{\gamma} = 0.1 \times 15^{1.4} = 4.431\ \text{MPa} \end{aligned}

Process 2–3 (heat added at constant pressure):

T3=T2+qscp=924.66+16751.005=2591.32 KT_3 = T_2 + \frac{q_s}{c_p} = 924.66 + \frac{1675}{1.005} = 2591.32\ \text{K}

Maximum temperature T3=2591.3T_3 = 2591.3 K; maximum pressure p3=p2=4.431p_3 = p_2 = 4.431 MPa.

(ii) Cut-off ratio

ρ=v3v2=T3T2=2591.32924.66=2.802\rho = \frac{v_3}{v_2} = \frac{T_3}{T_2} = \frac{2591.32}{924.66} = 2.802

(iii) Net work per kg of air

T4=T3(ρr)γ−1=2591.32(2.80215)0.4=1324.65 Kqr=cv(T4−T1)=0.718(1324.65−313)=726.37 kJ/kgWnet=qs−qr=1675−726.37=948.63 kJ/kg\begin{aligned} T_4 &= T_3\left(\frac{\rho}{r}\right)^{\gamma-1} = 2591.32\left(\frac{2.802}{15}\right)^{0.4} = 1324.65\ \text{K} \\ q_r &= c_v (T_4 - T_1) = 0.718(1324.65 - 313) = 726.37\ \text{kJ/kg} \\ W_{net} &= q_s - q_r = 1675 - 726.37 = 948.63\ \text{kJ/kg} \end{aligned}

(iv) Thermal efficiency

η=Wnetqs=948.631675=0.5664=56.64%\eta = \frac{W_{net}}{q_s} = \frac{948.63}{1675} = 0.5664 = 56.64\%

Check with the formula η=1−1rγ−1⋅ργ−1γ(ρ−1)=56.64%\eta = 1 - \dfrac{1}{r^{\gamma-1}}\cdot\dfrac{\rho^{\gamma}-1}{\gamma(\rho-1)} = 56.64\%.

(v) Mean effective pressure

v1=RT1p1=0.287×313100=0.8983 m3/kgv2=v1r=0.05989 m3/kgpm=Wnetv1−v2=948.630.8983−0.05989=1131.5 kPa\begin{aligned} v_1 &= \frac{R T_1}{p_1} = \frac{0.287 \times 313}{100} = 0.8983\ \text{m}^3/\text{kg} \\ v_2 &= \frac{v_1}{r} = 0.05989\ \text{m}^3/\text{kg} \\ p_m &= \frac{W_{net}}{v_1 - v_2} = \frac{948.63}{0.8983 - 0.05989} = 1131.5\ \text{kPa} \end{aligned}

Answer: TmaxT_{max} = 2591.3 K, pmaxp_{max} = 4.431 MPa, cut-off ratio = 2.802, WnetW_{net} = 948.6 kJ/kg, η\eta = 56.64 %, MEP = 1131.5 kPa ≈ 11.31 bar.

✓ Answer checked by Claude Opus 5.5 (high effort)

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