Calculate compression ratio, initial pressure, or final pressure using the ideal-gas isentropic relation and heat capacity ratio γ.

Compression Ratio to Pressure (Ideal-Gas Isentropic) Calculator

Enter any 2 of the 3 main values (CR, P₁, P₂) to calculate the missing one. γ defaults to 1.40 if left blank.






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Compression Ratio to Pressure Formula

The calculator uses the ideal-gas isentropic pressure relation. It assumes the compression process is adiabatic and reversible, with a constant heat capacity ratio, γ.

P_2 = P_1 * CR^\gamma
P_1 = P_2 / CR^\gamma
CR = (P_2 / P_1)^(1/\gamma)
  • P₁ = initial absolute pressure
  • P₂ = final absolute pressure after compression
  • CR = compression ratio, such as 10 for 10:1
  • γ = heat capacity ratio, also called the specific heat ratio

To calculate final pressure, enter compression ratio and initial pressure. The calculator applies P₂ = P₁ × CRγ.

To calculate initial pressure, enter compression ratio and final pressure. The calculator rearranges the same relation to P₁ = P₂ / CRγ.

To calculate compression ratio, enter the initial and final absolute pressures. The calculator solves CR = (P₂ / P₁)1/γ.

Pressure values must be absolute pressure, not gauge pressure. If you start with gauge pressure, add atmospheric pressure before using the value.

Typical Heat Capacity Ratio Values

For air at ordinary temperatures, γ is commonly taken as 1.40. Other gases can use different values.

Gas Typical γ Notes
Air 1.40 Default value for many compression estimates
Nitrogen 1.40 Very close to air for many calculations
Oxygen 1.40 Approximate room-temperature value
Carbon dioxide 1.30 Approximate value, varies with temperature
Helium 1.66 Monatomic gas

Pressure Unit Reference

Unit Equivalent in bar Equivalent in psi
1 bar 1 bar 14.5038 psi
1 atm 1.01325 bar 14.696 psi
1 kPa 0.01 bar 0.145038 psi
1 Pa 0.00001 bar 0.000145 psi

Examples

Example 1: Calculate final pressure from compression ratio

You have air with a compression ratio of 10:1, initial pressure of 1 atm absolute, and γ = 1.40.

P_2 = 1 * 10^1.40
P_2 = 25.1189 atm

The final pressure is about 25.12 atm absolute.

Example 2: Calculate compression ratio from pressure

You have an initial pressure of 1 bar absolute, a final pressure of 16 bar absolute, and γ = 1.40.

CR = (16 / 1)^(1/1.40)
CR = 7.2458

The compression ratio is about 7.25:1.

FAQ

Should I use absolute pressure or gauge pressure?

Use absolute pressure. The isentropic relation uses pressure ratios based on absolute pressure. If you have gauge pressure, add atmospheric pressure first. For example, 100 psi gauge is about 114.7 psi absolute at sea level.

Why does γ change the final pressure so much?

γ is the exponent in the formula P₂ = P₁ × CRγ. A higher γ produces a higher final pressure for the same compression ratio. For example, helium with γ around 1.66 gives a larger pressure rise than air with γ around 1.40.

Is this the same as real engine cylinder pressure?

Not exactly. This calculation is an ideal isentropic estimate. Real engine cylinder pressure depends on valve timing, heat loss, leakage, fuel mixture, combustion, temperature changes, and measurement conditions. Use this result as an ideal compression estimate, not as a full engine pressure prediction.