Turbine work in simple gas turbine cycle if temperature is known Calculator

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✖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 [C_p]			+10% -10%
✖Temperature at inlet of turbine is the measure of heat energy at the inlet of turbine.ⓘ Temperature at inlet of turbine [T₃]			+10% -10%
✖Temperature at the exit of turbine is the measure of heat energy at the exit of turbine.ⓘ Temperature at the exit of turbine [T₄]			+10% -10%

✖Work Done by turbine is the amount of work output obtained from turbine.ⓘ Turbine work in simple gas turbine cycle if temperature is known [W_T]

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Turbine work in simple gas turbine cycle if temperature is known

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!

< 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

< 1 Other formulas that calculate the same Output

Turbine work in simple gas turbine cycle

Work Done by turbine=Enthalpy at inlet of turbine-Enthalpy at exit of turbine GO

Turbine work in simple gas turbine cycle if temperature is known Formula

Work Done by turbine=Specific Heat Capacity at Constant Pressure*(Temperature at inlet of turbine-Temperature at the exit of turbine)
WT=Cp*(T3-T4)

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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 if temperature is known?

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

How to calculate Turbine work in simple gas turbine cycle if temperature is known using this online calculator? To use this online calculator for Turbine work in simple gas turbine cycle if temperature is known, enter Specific Heat Capacity at Constant Pressure (C_p), Temperature at inlet of turbine (T₃) and Temperature at the exit of turbine (T₄) and hit the calculate button. Here is how the Turbine work in simple gas turbine cycle if temperature is known calculation can be explained with given input values -> 0.264 = 8*(48-15).

FAQ

What is Turbine work in simple gas turbine cycle if temperature is known?

The Turbine work in simple gas turbine cycle if temperature is known formula is defined as the product of specific heat at constant pressure and difference of temperatures at inlet and exit of turbine and is represented as W_T=C_p*(T₃-T₄) or Work Done by turbine=Specific Heat Capacity at Constant Pressure*(Temperature at inlet of turbine-Temperature at the exit of turbine). 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, Temperature at inlet of turbine is the measure of heat energy at the inlet of turbine and Temperature at the exit of turbine is the measure of heat energy at the exit of turbine.

How to calculate Turbine work in simple gas turbine cycle if temperature is known?

The Turbine work in simple gas turbine cycle if temperature is known formula is defined as the product of specific heat at constant pressure and difference of temperatures at inlet and exit of turbine is calculated using Work Done by turbine=Specific Heat Capacity at Constant Pressure*(Temperature at inlet of turbine-Temperature at the exit of turbine). To calculate Turbine work in simple gas turbine cycle if temperature is known, you need Specific Heat Capacity at Constant Pressure (C_p), Temperature at inlet of turbine (T₃) and Temperature at the exit of turbine (T₄). With our tool, you need to enter the respective value for Specific Heat Capacity at Constant Pressure, Temperature at inlet of turbine and Temperature at the 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 Specific Heat Capacity at Constant Pressure, Temperature at inlet of turbine and Temperature at the exit of turbine. We can use 1 other way(s) to calculate the same, which is/are as follows -

Work Done by turbine=Enthalpy at inlet of turbine-Enthalpy at exit of turbine

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