Net work output in simple gas turbine cycle Formula

Fx Copy
LaTeX Copy
Net Work Output is defined as the difference of work of turbine and work of compressor. Check FAQs
WNet=Cp((T3-T4)-(T2-T1))
WNet - Net Work Output?Cp - Specific Heat Capacity at Constant Pressure?T3 - Temperature at Inlet of Turbine?T4 - Temperature at Exit of Turbine?T2 - Temperature at Exit of Compressor?T1 - Temperature at Inlet of Compressor?

Net work output in simple gas turbine cycle Example

With values
With units
Only example

Here is how the Net work output in simple gas turbine cycle equation looks like with Values.

Here is how the Net work output in simple gas turbine cycle equation looks like with Units.

Here is how the Net work output in simple gas turbine cycle equation looks like.

57.408Edit=1.248Edit((555Edit-439Edit)-(370Edit-300Edit))
You are here -
HomeIcon Home » Category Physics » Category Aerospace » Category Propulsion » fx Net work output in simple gas turbine cycle

Net work output in simple gas turbine cycle Solution

Follow our step by step solution on how to calculate Net work output in simple gas turbine cycle?

FIRST Step Consider the formula
WNet=Cp((T3-T4)-(T2-T1))
Next Step Substitute values of Variables
WNet=1.248kJ/kg*K((555K-439K)-(370K-300K))
Next Step Convert Units
WNet=1248J/(kg*K)((555K-439K)-(370K-300K))
Next Step Prepare to Evaluate
WNet=1248((555-439)-(370-300))
Next Step Evaluate
WNet=57408J
LAST Step Convert to Output's Unit
WNet=57.408KJ

Net work output in simple gas turbine cycle Formula Elements

Variables
Net Work Output
Net Work Output is defined as the difference of work of turbine and work of compressor.
Symbol: WNet
Measurement: EnergyUnit: KJ
Note: Value can be positive or negative.
Specific Heat Capacity at Constant Pressure
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.
Symbol: Cp
Measurement: Specific Heat CapacityUnit: kJ/kg*K
Note: Value can be positive or negative.
Temperature at Inlet of Turbine
The Temperature at Inlet of Turbine is used to measure the amount of heat energy at the entry of the Turbine.
Symbol: T3
Measurement: TemperatureUnit: K
Note: Value should be greater than 0.
Temperature at Exit of Turbine
The Temperature at Exit of Turbine is used to measure the amount of heat energy at the exit of the Turbine.
Symbol: T4
Measurement: TemperatureUnit: K
Note: Value should be greater than 0.
Temperature at Exit of Compressor
The Temperature at Exit of Compressor is used to measure the amount of heat energy at the exit of the compressor.
Symbol: T2
Measurement: TemperatureUnit: K
Note: Value can be positive or negative.
Temperature at Inlet of Compressor
The Temperature at Inlet of Compressor is used to measure the amount of heat energy at the entry of the compressor.
Symbol: T1
Measurement: TemperatureUnit: K
Note: Value can be positive or negative.

Other formulas in Efficiency Metrics category

​Go Isentropic Efficiency of Expansion Machine
ηT=WactualWs,out
​Go Propulsive power
P=12((ma+mf)Ve2-(maV2))
​Go Thermal Efficiency of Jet Engines given Effective Speed Ratio
ηth=Ve2(1-α2)2fQ
​Go Transmission Efficiency given Output and Input of Transmission
ηtransmission=PoutPin

How to Evaluate Net work output in simple gas turbine cycle?

Net work output in simple gas turbine cycle evaluator uses Net Work Output = Specific Heat Capacity at Constant Pressure*((Temperature at Inlet of Turbine-Temperature at Exit of Turbine)-(Temperature at Exit of Compressor-Temperature at Inlet of Compressor)) to evaluate the Net Work Output, Net work output in simple gas turbine cycle is a measure of the net energy produced by a simple gas turbine cycle, which is a type of heat engine that converts the energy released from burning fuel into mechanical energy. It is an important parameter in evaluating the performance of a gas turbine cycle. Net Work Output is denoted by WNet symbol.

How to evaluate Net work output in simple gas turbine cycle using this online evaluator? To use this online evaluator for Net work output in simple gas turbine cycle, enter Specific Heat Capacity at Constant Pressure (Cp), Temperature at Inlet of Turbine (T3), Temperature at Exit of Turbine (T4), Temperature at Exit of Compressor (T2) & Temperature at Inlet of Compressor (T1) and hit the calculate button.

FAQs on Net work output in simple gas turbine cycle

What is the formula to find Net work output in simple gas turbine cycle?
The formula of Net work output in simple gas turbine cycle is expressed as Net Work Output = Specific Heat Capacity at Constant Pressure*((Temperature at Inlet of Turbine-Temperature at Exit of Turbine)-(Temperature at Exit of Compressor-Temperature at Inlet of Compressor)). Here is an example- 0.047424 = 1248*((555-439)-(370-300)).
How to calculate Net work output in simple gas turbine cycle?
With Specific Heat Capacity at Constant Pressure (Cp), Temperature at Inlet of Turbine (T3), Temperature at Exit of Turbine (T4), Temperature at Exit of Compressor (T2) & Temperature at Inlet of Compressor (T1) we can find Net work output in simple gas turbine cycle using the formula - Net Work Output = Specific Heat Capacity at Constant Pressure*((Temperature at Inlet of Turbine-Temperature at Exit of Turbine)-(Temperature at Exit of Compressor-Temperature at Inlet of Compressor)).
Can the Net work output in simple gas turbine cycle be negative?
Yes, the Net work output in simple gas turbine cycle, measured in Energy can be negative.
Which unit is used to measure Net work output in simple gas turbine cycle?
Net work output in simple gas turbine cycle is usually measured using the Kilojoule[KJ] for Energy. Joule[KJ], Gigajoule[KJ], Megajoule[KJ] are the few other units in which Net work output in simple gas turbine cycle can be measured.
Copied!