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Isentropic Efficiency of Compressor is the ratio of isentropic work of compressor to actual work of compressor. Check FAQs
ηC=T2-T1T2,actual-T1
ηC - Isentropic Efficiency of Compressor?T2 - Temperature at Compressor Exit?T1 - Temperature at Compressor Inlet?T2,actual - Actual Temperature at Compressor Exit?

Efficiency of compressor in actual gas turbine cycle Example

With values
With units
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Here is how the Efficiency of compressor in actual gas turbine cycle equation looks like with Values.

Here is how the Efficiency of compressor in actual gas turbine cycle equation looks like with Units.

Here is how the Efficiency of compressor in actual gas turbine cycle equation looks like.

0.9242Edit=420Edit-298.15Edit430Edit-298.15Edit
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Efficiency of compressor in actual gas turbine cycle Solution

Follow our step by step solution on how to calculate Efficiency of compressor in actual gas turbine cycle?

FIRST Step Consider the formula
ηC=T2-T1T2,actual-T1
Next Step Substitute values of Variables
ηC=420K-298.15K430K-298.15K
Next Step Prepare to Evaluate
ηC=420-298.15430-298.15
Next Step Evaluate
ηC=0.924156238149412
LAST Step Rounding Answer
ηC=0.9242

Efficiency of compressor in actual gas turbine cycle Formula Elements

Variables
Isentropic Efficiency of Compressor
Isentropic Efficiency of Compressor is the ratio of isentropic work of compressor to actual work of compressor.
Symbol: ηC
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Temperature at Compressor Exit
Temperature at Compressor Exit is the temperature of the gases exiting the compressor.
Symbol: T2
Measurement: TemperatureUnit: K
Note: Value should be greater than 0.
Temperature at Compressor Inlet
Temperature at Compressor Inlet is the temperature of the gases entering the compressor.
Symbol: T1
Measurement: TemperatureUnit: K
Note: Value should be greater than 0.
Actual Temperature at Compressor Exit
Actual Temperature at Compressor Exit is the temperature of the gases exiting the compressor considering the losses throughout the compression process.
Symbol: T2,actual
Measurement: TemperatureUnit: K
Note: Value should be greater than 0.

Other Formulas to find Isentropic Efficiency of Compressor

​Go Isentropic Efficiency of Compression Machine
ηC=Ws,inWin
​Go Efficiency of Compressor given Enthalpy
ηC=h2,ideal-h1h2,actual-h1

Other formulas in Compressor category

​Go Degree of Reaction for Compressor
R=ΔErotor increaseΔEstage increase
​Go Mean Diameter of Impeller
Dm=Dt2+Dh22
​Go Tip Velocity of Impeller given Mean Diameter
Ut=π(2Dm2-Dh2)0.5N60
​Go Tip Velocity of Impeller given Hub Diameter
Ut=πN60Dt2+Dh22

How to Evaluate Efficiency of compressor in actual gas turbine cycle?

Efficiency of compressor in actual gas turbine cycle evaluator uses Isentropic Efficiency of Compressor = (Temperature at Compressor Exit-Temperature at Compressor Inlet)/(Actual Temperature at Compressor Exit-Temperature at Compressor Inlet) to evaluate the Isentropic Efficiency of Compressor, The Efficiency of Compressor in Actual Gas Turbine Cycle measures how effectively the compressor increases the temperature of the air compared to the theoretical maximum. This formula calculates the isentropic efficiency by comparing the temperature rise in the compressor under actual conditions to the temperature rise in an ideal, isentropic process. Isentropic Efficiency of Compressor is denoted by ηC symbol.

How to evaluate Efficiency of compressor in actual gas turbine cycle using this online evaluator? To use this online evaluator for Efficiency of compressor in actual gas turbine cycle, enter Temperature at Compressor Exit (T2), Temperature at Compressor Inlet (T1) & Actual Temperature at Compressor Exit (T2,actual) and hit the calculate button.

FAQs on Efficiency of compressor in actual gas turbine cycle

What is the formula to find Efficiency of compressor in actual gas turbine cycle?
The formula of Efficiency of compressor in actual gas turbine cycle is expressed as Isentropic Efficiency of Compressor = (Temperature at Compressor Exit-Temperature at Compressor Inlet)/(Actual Temperature at Compressor Exit-Temperature at Compressor Inlet). Here is an example- 0.924156 = (420-298.15)/(430-298.15).
How to calculate Efficiency of compressor in actual gas turbine cycle?
With Temperature at Compressor Exit (T2), Temperature at Compressor Inlet (T1) & Actual Temperature at Compressor Exit (T2,actual) we can find Efficiency of compressor in actual gas turbine cycle using the formula - Isentropic Efficiency of Compressor = (Temperature at Compressor Exit-Temperature at Compressor Inlet)/(Actual Temperature at Compressor Exit-Temperature at Compressor Inlet).
What are the other ways to Calculate Isentropic Efficiency of Compressor?
Here are the different ways to Calculate Isentropic Efficiency of Compressor-
  • Isentropic Efficiency of Compressor=Isentropic Work Input/Actual Work InputOpenImg
  • Isentropic Efficiency of Compressor=(Ideal Enthalpy after Compression-Enthalpy at Compressor Inlet)/(Actual Enthalpy after Compression-Enthalpy at Compressor Inlet)OpenImg
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