Pressure Ratio Solution

STEP 0: Pre-Calculation Summary
Formula Used
Pressure Ratio = Final Pressure/Initial Pressure
PR = Pf/Pi
This formula uses 3 Variables
Variables Used
Pressure Ratio - Pressure Ratio is ratio of final to initial pressure.
Final Pressure - (Measured in Pascal) - Final Pressure is the pressure of a fluid or gas at the conclusion of a process or within a system.
Initial Pressure - (Measured in Pascal) - Initial Pressure refers to the pressure of a fluid or gas at the beginning of a process or within a system.
STEP 1: Convert Input(s) to Base Unit
Final Pressure: 259 Pascal --> 259 Pascal No Conversion Required
Initial Pressure: 65 Pascal --> 65 Pascal No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
PR = Pf/Pi --> 259/65
Evaluating ... ...
PR = 3.98461538461538
STEP 3: Convert Result to Output's Unit
3.98461538461538 --> No Conversion Required
FINAL ANSWER
3.98461538461538 3.984615 <-- Pressure Ratio
(Calculation completed in 00.004 seconds)

Credits

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Created by Chilvera Bhanu Teja
Institute of Aeronautical Engineering (IARE), Hyderabad
Chilvera Bhanu Teja has created this Calculator and 300+ more calculators!
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Verified by Sagar S Kulkarni
Dayananda Sagar College of Engineering (DSCE), Bengaluru
Sagar S Kulkarni has verified this Calculator and 200+ more calculators!

19 Thermodynamics and Governing Equations Calculators

Max work output in Brayton cycle
​ Go Maximum Work done in Brayton Cycle = (1005*1/Compressor Efficiency)*Temperature at Inlet of Compressor in Brayton*(sqrt(Temperature at Inlet to Turbine in Brayton Cycle/Temperature at Inlet of Compressor in Brayton*Compressor Efficiency*Turbine Efficiency)-1)^2
Choked Mass Flow Rate given specific heat ratio
​ Go Choked Mass Flow Rate = (Heat Capacity Ratio/(sqrt(Heat Capacity Ratio-1)))*((Heat Capacity Ratio+1)/2)^(-((Heat Capacity Ratio+1)/(2*Heat Capacity Ratio-2)))
Choked Mass Flow Rate
​ Go Choked Mass Flow Rate = (Mass Flow Rate*sqrt(Specific Heat Capacity at Constant Pressure*Temperature))/(Nozzle Throat Area*Throat Pressure)
Stagnation Velocity of Sound given Specific Heat at Constant Pressure
​ Go Stagnation Velocity of Sound = sqrt((Heat Capacity Ratio-1)*Specific Heat Capacity at Constant Pressure*Stagnation Temperature)
Specific Heat of mixed out gas
​ Go Specific Heat of Mixed Gas = (Specific Heat of Core Gas+Bypass Ratio*Specific Heat of Bypass Air)/(1+Bypass Ratio)
Stagnation Temperature
​ Go Stagnation Temperature = Static Temperature+(Flow Velocity Downstream of Sound^2)/(2*Specific Heat Capacity at Constant Pressure)
Stagnation Velocity of Sound
​ Go Stagnation Velocity of Sound = sqrt(Heat Capacity Ratio*[R]*Stagnation Temperature)
Speed of Sound
​ Go Speed of Sound = sqrt(Specific Heat Ratio*[R-Dry-Air]*Static Temperature)
Stagnation Velocity of Sound given Stagnation Enthalpy
​ Go Stagnation Velocity of Sound = sqrt((Heat Capacity Ratio-1)*Stagnation Enthalpy)
Heat Capacity Ratio
​ Go Heat Capacity Ratio = Specific Heat Capacity at Constant Pressure/Specific Heat Capacity at Constant Volume
Efficiency of cycle
​ Go Efficiency of Cycle = (Turbine Work-Compressor Work)/Heat
Internal Energy of Perfect Gas at given Temperature
​ Go Internal Energy = Specific Heat Capacity at Constant Volume*Temperature
Enthalpy of Ideal Gas at given Temperature
​ Go Enthalpy = Specific Heat Capacity at Constant Pressure*Temperature
Stagnation enthalpy
​ Go Stagnation Enthalpy = Enthalpy+(Velocity of Fluid Flow^2)/2
Efficiency of Joule cycle
​ Go Efficiency of Joule Cycle = Net Work Output/Heat
Pressure Ratio
​ Go Pressure Ratio = Final Pressure/Initial Pressure
Work ratio in practical cycle
​ Go Work Ratio = 1-(Compressor Work/Turbine Work)
Mach Number
​ Go Mach Number = Speed of Object/Speed of Sound
Mach Angle
​ Go Mach Angle = asin(1/Mach Number)

Pressure Ratio Formula

Pressure Ratio = Final Pressure/Initial Pressure
PR = Pf/Pi

What is pressure ratio?

Pressure ratio is the ratio of final pressure after process to the initial pressure before process. It gives the degree with which gas is compressed.

How to Calculate Pressure Ratio?

Pressure Ratio calculator uses Pressure Ratio = Final Pressure/Initial Pressure to calculate the Pressure Ratio, The Pressure ratio formula is defined as the ratio of the final pressure after process to the initial pressure before process. Pressure Ratio is denoted by PR symbol.

How to calculate Pressure Ratio using this online calculator? To use this online calculator for Pressure Ratio, enter Final Pressure (Pf) & Initial Pressure (Pi) and hit the calculate button. Here is how the Pressure Ratio calculation can be explained with given input values -> 3.984615 = 259/65.

FAQ

What is Pressure Ratio?
The Pressure ratio formula is defined as the ratio of the final pressure after process to the initial pressure before process and is represented as PR = Pf/Pi or Pressure Ratio = Final Pressure/Initial Pressure. Final Pressure is the pressure of a fluid or gas at the conclusion of a process or within a system & Initial Pressure refers to the pressure of a fluid or gas at the beginning of a process or within a system.
How to calculate Pressure Ratio?
The Pressure ratio formula is defined as the ratio of the final pressure after process to the initial pressure before process is calculated using Pressure Ratio = Final Pressure/Initial Pressure. To calculate Pressure Ratio, you need Final Pressure (Pf) & Initial Pressure (Pi). With our tool, you need to enter the respective value for Final Pressure & Initial Pressure and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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