Air is the working fluid with R = 0.287 kJ/(kg·K). The constant-volume specific heat c_v is computed from γ as c_v = R/(γ−1).
X axis = specific volume v (relative to v₁=1) / Y axis = pressure P (relative to P₁=1) / yellow shaded area = net work
X axis = compression ratio r / Y axis = thermal efficiency η (yellow dot = current r, dashed = current η)
The Otto cycle is the air-standard idealization of a spark-ignition engine, made up of four processes: isentropic compression (1→2), constant-volume heat addition (2→3), isentropic expansion (3→4) and constant-volume heat rejection (4→1).
Thermal efficiency η depends only on the compression ratio r and the specific heat ratio γ:
$$\eta = 1 - \frac{1}{r^{\gamma-1}}$$End-of-compression temperature T₂ and after-combustion temperature T₃. Here c_v is the constant-volume specific heat (c_v = R/(γ−1)):
$$T_2 = T_1\,r^{\gamma-1}, \qquad T_3 = T_2 + \frac{Q_\text{in}}{c_v}$$End-of-expansion temperature T₄ and net work w_net:
$$T_4 = \frac{T_3}{r^{\gamma-1}}, \qquad w_\text{net} = \eta\,Q_\text{in}$$Efficiency does not depend on the heat input Q_in and rises with the compression ratio r. Real gasoline engines are limited to roughly r = 9 to 12 by knock.