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Thermodynamics Tool

Thermodynamic Cycle Calculator

Visualize Carnot, Otto, Diesel, and Brayton cycles on P-V and T-s diagrams in real time. Instantly compute thermal efficiency, net work, and heat exchange quantities.

$$\eta = 1 - \frac{Q_L}{Q_H} = 1 - \frac{T_L}{T_H} \text{ (Carnot)}$$
Parameters
Cycle Type
Heat capacity ratio γ 1.40
Air: 1.40 / Monatomic ideal gas: 1.67
Cold reservoir T_L / Inlet temperature T₁ [K] 300 K
Hot reservoir T_H / Peak temperature T₃ [K] 1200 K
Compression ratio r_c 9.0
Otto: 8–12 / Diesel: 14–22
Initial pressure p₁ [kPa] 101 kPa
Otto Cycle
Ideal cycle for gasoline engines, assuming constant-volume combustion.
Theoretical efficiency is higher than the practical 30–35% of real engines.
Thermal efficiency η
%
Net work W_net
kJ/kg
Heat input Q_in
kJ/kg
Heat rejected Q_out
kJ/kg
State 1
State 2
State 3
State 4
P-V Diagram (Equation of State)
T-s Diagram (Entropy)
Theory — Thermodynamic Cycle Efficiency Formulas

Carnot Efficiency (Theoretical Upper Limit)

$$\eta_\text{Carnot} = 1 - \frac{T_L}{T_H}$$

The highest efficiency achievable by any reversible cycle operating between the same two temperature reservoirs.

Otto Efficiency

$$\eta_\text{Otto} = 1 - \frac{1}{r_c^{\,\gamma-1}}$$

Determined by compression ratio $r_c = V_1/V_2$. Example: $r_c=9, \gamma=1.4$ → η ≈ 58%

Diesel Efficiency

$$\eta_\text{Diesel} = 1 - \frac{1}{r_c^{\gamma-1}}\cdot\frac{r_\text{CO}^\gamma - 1}{\gamma(r_\text{CO}-1)}$$

Characterized by high compression ratio and constant-pressure combustion.

Brayton Efficiency

$$\eta_\text{Brayton} = 1 - r_p^{\,(1-\gamma)/\gamma}$$

Determined by pressure ratio $r_p$. The fundamental cycle for gas turbines and jet engines.