Enter the initial pressure, initial volume, final pressure, final volume, and adiabatic index into the calculator to determine the missing variable in an adiabatic process.

Adiabatic Pressure Calculator

Enter any 4 values to calculate the missing variable

Adiabatic Pressure Formula

The following formula is used to calculate the pressure or volume in an adiabatic process.

P_1 \cdot V_1^\gamma = P_2 \cdot V_2^\gamma

Variables:

  • (P_1) is the initial pressure
  • (V_1) is the initial volume
  • (P_2) is the final pressure
  • (V_2) is the final volume
  • (gamma) is the adiabatic index

To calculate the missing variable in an adiabatic process, use the formula above and solve for the unknown variable. The adiabatic index ((gamma)) is a constant that depends on the specific gas and its properties.

What is an Adiabatic Process?

An adiabatic process is a thermodynamic process in which there is no heat exchange between the system and its surroundings. This means that all the work done on or by the system results in a change in the internal energy of the system. In an adiabatic process, the temperature of the system can change even though no heat is added or removed. Adiabatic processes are commonly found in various natural and engineering systems, such as in the compression and expansion of gases in engines and refrigeration cycles.

How to Calculate Adiabatic Pressure?

The following steps outline how to calculate the adiabatic pressure or volume.


  1. First, determine the initial pressure ((P_1)) and initial volume ((V_1)).
  2. Next, determine the final pressure ((P_2)) and final volume ((V_2)).
  3. Next, determine the adiabatic index ((gamma)).
  4. Use the formula (P_1 cdot V_1^gamma = P_2 cdot V_2^gamma) to solve for the unknown variable.
  5. After inserting the values and calculating the result, check your answer with the calculator above.

Example Problem : 

Use the following variables as an example problem to test your knowledge.

Initial Pressure ((P_1)) = 100 kPa

Initial Volume ((V_1)) = 1 m³

Final Pressure ((P_2)) = 200 kPa

Adiabatic Index ((gamma)) = 1.4