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Compressor work in simple gas turbine if temperature is known Calculator

Category Physics ↺
Physics Gas Turbines ↺
Gas-Turbines Gas cycles ↺
Gas-Cycles Ideal cycles ↺
✖Specific heat capacity at constant pressure means the amount of heat that is required to raise the temperature of a unit mass of gas by 1 degree at constant pressure.ⓘ Specific Heat Capacity at Constant Pressure [Cp]
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✖Exit temperature is the degree of measure of heat at exit to the system.ⓘ Exit temperature [Texit]
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-10%
✖Inlet temperature is the degree of measure of heat at inlet to the system.ⓘ Inlet temperature [Tinlet]
+10%
-10%
✖Compressor work is the work done by the compressor.ⓘ Compressor work in simple gas turbine if temperature is known [Wc]
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Chilvera Bhanu Teja
Institute of Aeronautical Engineering (IARE), Hyderabad
Chilvera Bhanu Teja has created this Calculator and 200+ more calculators!
Vaibhav Malani
National Institute of Technology (NIT), Tiruchirapalli
Vaibhav Malani has verified this Calculator and 100+ more calculators!

11 Other formulas that you can solve using the same Inputs

Power required to maintain pressure inside the cabin(excluding ram work)
Input Power=((Mass of air*Specific Heat Capacity at Constant Pressure*Actual temperature of Rammed Air)/(Compressor efficiency))*((Cabin Pressure/Pressure of rammed air)^((Heat Capacity Ratio-1)/Heat Capacity Ratio)-1) GO
Power required to maintain pressure inside the cabin(including ram work)
Input Power=((Mass of air*Specific Heat Capacity at Constant Pressure*Ambient air temperature)/(Compressor efficiency))*((Cabin Pressure/Atmospheric Pressure)^((Heat Capacity Ratio-1)/Heat Capacity Ratio)-1) GO
Mass of air to produce Q tonnes of refrigeration
Mass of air=(210*Tonnage of Refrigeration)/(1000*Specific Heat Capacity at Constant Pressure*(Temperature at the end of Isentropic Expansion-Actual exit Temperature of cooling turbine)) GO
Mass of air to produce Q tonnes of refrigeration
Mass of air=(210*Tonnage of Refrigeration)/(Specific Heat Capacity at Constant Pressure*(Inside temperature of cabin-Actual temperature at end of isentropic expansion)) GO
Refrigeration Effect Produced
Refrigeration Effect Produced=Mass of air*Specific Heat Capacity at Constant Pressure*(Inside temperature of cabin-Actual temperature at end of isentropic expansion) GO
Heat Absorbed during Constant pressure Expansion Process
Heat Absorbed=Specific Heat Capacity at Constant Pressure*(Temperature at the start of Isentropic Compression-Temperature at the end of Isentropic Expansion) GO
Heat rejected during cooling process
Heat Rejected=Mass of air*Specific Heat Capacity at Constant Pressure*(Actual end temp of isentropic compression-Temperature at the end of cooling process) GO
Expansion Work
Work =Mass of air*Specific Heat Capacity at Constant Pressure*(Temperature at the end of cooling process-Actual temperature at end of isentropic expansion) GO
Power required for refrigeration system
Input Power=(Mass of air*Specific Heat Capacity at Constant Pressure*(Actual end temp of isentropic compression-Actual temperature of Rammed Air))/60 GO
Heat Rejected during Constant pressure Cooling Process
Heat Rejected=Specific Heat Capacity at Constant Pressure*(Ideal temp at end of isentropic compression-Ideal temp at the end of isobaric cooling) GO
Compression Work
Work =Mass of air*Specific Heat Capacity at Constant Pressure*(Actual end temp of isentropic compression-Actual temperature of Rammed Air) GO

2 Other formulas that calculate the same Output

Work required to drive the compressor including mechanical losses
Compressor work=(1/Mechanical Efficiency)*Specific heat at constant pressure*(Actual end temp of isentropic compression-Temperature at inlet of compressor) GO
Compressor work
Compressor work=Enthalpy after compression-Enthalpy before compression GO

Compressor work in simple gas turbine if temperature is known Formula

Compressor work=Specific Heat Capacity at Constant Pressure*(Exit temperature-Inlet temperature)
W<sub>c</sub>=C<sub>p</sub>*(T<sub>exit</sub>-T<sub>inlet</sub>)
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How does compressor work?

Compressors work by forcing air into a container and pressurizing it. Then, the air is forced through an opening in the tank, where pressure builds up.

How to Calculate Compressor work in simple gas turbine if temperature is known?

Compressor work in simple gas turbine if temperature is known calculator uses Compressor work=Specific Heat Capacity at Constant Pressure*(Exit temperature-Inlet temperature) to calculate the Compressor work, The Compressor work in simple gas turbine if temperature is known formula is defined as the product of specific heat at constant pressure and difference of inlet and exit temperatures of compressor. Compressor work and is denoted by Wc symbol.

How to calculate Compressor work in simple gas turbine if temperature is known using this online calculator? To use this online calculator for Compressor work in simple gas turbine if temperature is known, enter Specific Heat Capacity at Constant Pressure (Cp), Exit temperature (Texit) and Inlet temperature (Tinlet) and hit the calculate button. Here is how the Compressor work in simple gas turbine if temperature is known calculation can be explained with given input values -> 0.264 = 8*(48-15).

FAQ

What is Compressor work in simple gas turbine if temperature is known?
The Compressor work in simple gas turbine if temperature is known formula is defined as the product of specific heat at constant pressure and difference of inlet and exit temperatures of compressor and is represented as Wc=Cp*(Texit-Tinlet) or Compressor work=Specific Heat Capacity at Constant Pressure*(Exit temperature-Inlet temperature). Specific heat capacity at constant pressure means the amount of heat that is required to raise the temperature of a unit mass of gas by 1 degree at constant pressure, Exit temperature is the degree of measure of heat at exit to the system and Inlet temperature is the degree of measure of heat at inlet to the system.
How to calculate Compressor work in simple gas turbine if temperature is known?
The Compressor work in simple gas turbine if temperature is known formula is defined as the product of specific heat at constant pressure and difference of inlet and exit temperatures of compressor is calculated using Compressor work=Specific Heat Capacity at Constant Pressure*(Exit temperature-Inlet temperature). To calculate Compressor work in simple gas turbine if temperature is known, you need Specific Heat Capacity at Constant Pressure (Cp), Exit temperature (Texit) and Inlet temperature (Tinlet). With our tool, you need to enter the respective value for Specific Heat Capacity at Constant Pressure, Exit temperature and Inlet temperature and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Compressor work?
In this formula, Compressor work uses Specific Heat Capacity at Constant Pressure, Exit temperature and Inlet temperature. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Compressor work=Enthalpy after compression-Enthalpy before compression
  • Compressor work=(1/Mechanical Efficiency)*Specific heat at constant pressure*(Actual end temp of isentropic compression-Temperature at inlet of compressor)
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