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

2 Other formulas that you can solve using the same Inputs

Efficiency of turbine in actual gas turbine cycle in terms of enthalpy
Efficiency of turbine=(Enthalpy at inlet of turbine-Enthalpy at exit of turbine in actual cycle)/(Enthalpy at inlet of turbine-Enthalpy at exit of turbine in ideal cycle) GO
Amount of heat added in simple gas turbine cycle if temperature is known
Heat added=Specific Heat Capacity at Constant Pressure*(Enthalpy at exit of turbine-Inlet temperature) GO

2 Other formulas that calculate the same Output

Work of turbine without pressure losses
Work Done by turbine=Efficiency of turbine*Specific heat at constant pressure*Temperature at inlet of turbine*((pressure ratio^((Heat Capacity Ratio-1)/Heat Capacity Ratio)-1)/(pressure ratio^((Heat Capacity Ratio-1)/Heat Capacity Ratio))) GO
Turbine work in simple gas turbine cycle if temperature is known
Work Done by turbine=Specific Heat Capacity at Constant Pressure*(Temperature at inlet of turbine-Temperature at the exit of turbine) GO

Turbine work in simple gas turbine cycle Formula

Work Done by turbine=Enthalpy at inlet of turbine-Enthalpy at exit of turbine
W<sub>T</sub>=h<sub>3</sub>-h<sub>4</sub>
More formulas
Compressor work GO
Amount of heat added in simple gas turbine cycle GO
Net work output in simple gas turbine cycle GO
Compressor work in simple gas turbine if temperature is known GO
Amount of heat added in simple gas turbine cycle if temperature is known GO
Turbine work in simple gas turbine cycle if temperature is known GO
Efficiency of a Joule cycle GO
Efficiency of cycle GO

What is work done?

Work done is a process, where energy given as input to the system is utilized to perform some useful work.

How to Calculate Turbine work in simple gas turbine cycle?

Turbine work in simple gas turbine cycle calculator uses Work Done by turbine=Enthalpy at inlet of turbine-Enthalpy at exit of turbine to calculate the Work Done by turbine, The Turbine work in simple gas turbine cycle formula is defined as the difference between enthalpy at inlet of turbine and enthalpy at exit of turbine. Work Done by turbine and is denoted by WT symbol.

How to calculate Turbine work in simple gas turbine cycle using this online calculator? To use this online calculator for Turbine work in simple gas turbine cycle, enter Enthalpy at inlet of turbine (h3) and Enthalpy at exit of turbine (h4) and hit the calculate button. Here is how the Turbine work in simple gas turbine cycle calculation can be explained with given input values -> 200 = 248000-48000.

FAQ

What is Turbine work in simple gas turbine cycle?
The Turbine work in simple gas turbine cycle formula is defined as the difference between enthalpy at inlet of turbine and enthalpy at exit of turbine and is represented as WT=h3-h4 or Work Done by turbine=Enthalpy at inlet of turbine-Enthalpy at exit of turbine. Enthalpy at inlet of turbine is the energy which is input to turbine and Enthalpy at exit of turbine is the energy which got out from the turbine.
How to calculate Turbine work in simple gas turbine cycle?
The Turbine work in simple gas turbine cycle formula is defined as the difference between enthalpy at inlet of turbine and enthalpy at exit of turbine is calculated using Work Done by turbine=Enthalpy at inlet of turbine-Enthalpy at exit of turbine. To calculate Turbine work in simple gas turbine cycle, you need Enthalpy at inlet of turbine (h3) and Enthalpy at exit of turbine (h4). With our tool, you need to enter the respective value for Enthalpy at inlet of turbine and Enthalpy at exit of turbine 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 Work Done by turbine?
In this formula, Work Done by turbine uses Enthalpy at inlet of turbine and Enthalpy at exit of turbine. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Work Done by turbine=Specific Heat Capacity at Constant Pressure*(Temperature at inlet of turbine-Temperature at the exit of turbine)
  • Work Done by turbine=Efficiency of turbine*Specific heat at constant pressure*Temperature at inlet of turbine*((pressure ratio^((Heat Capacity Ratio-1)/Heat Capacity Ratio)-1)/(pressure ratio^((Heat Capacity Ratio-1)/Heat Capacity Ratio)))
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