Thermal Efficiency of Propeller Engines Calculator

✖Break power is power developed at the output shaft.ⓘ Break Power [BP]			+10% -10%
✖Fuel Flow Rate is the fuel mass flow rate.ⓘ Fuel Flow Rate [m_f]			+10% -10%
✖Fuel Calorific Value denotes the amount of heat energy released per unit mass of fuel upon complete combustion.ⓘ Fuel Calorific Value [Q]			+10% -10%

✖Thermal Efficiency signifies the ratio of the work output of a turboprop engine to the heat input from fuel.ⓘ Thermal Efficiency of Propeller Engines [η_th]

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Thermal Efficiency of Propeller Engines Solution

STEP 0: Pre-Calculation Summary

Formula Used

Thermal Efficiency = Break Power/(Fuel Flow Rate*Fuel Calorific Value)
η_th = BP/(m_f*Q)
This formula uses 4 Variables

Variables Used

Thermal Efficiency - Thermal Efficiency signifies the ratio of the work output of a turboprop engine to the heat input from fuel.
Break Power - (Measured in Watt) - Break power is power developed at the output shaft.
Fuel Flow Rate - (Measured in Kilogram per Second) - Fuel Flow Rate is the fuel mass flow rate.
Fuel Calorific Value - (Measured in Joule per Kilogram) - Fuel Calorific Value denotes the amount of heat energy released per unit mass of fuel upon complete combustion.

STEP 1: Convert Input(s) to Base Unit

Break Power: 125 Kilowatt --> 125000 Watt (Check conversion here)
Fuel Flow Rate: 0.05 Kilogram per Second --> 0.05 Kilogram per Second No Conversion Required
Fuel Calorific Value: 43510 Kilojoule per Kilogram --> 43510000 Joule per Kilogram (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

η_th = BP/(m_f*Q) --> 125000/(0.05*43510000)

Evaluating ... ...

η_th = 0.0574580556193978

STEP 3: Convert Result to Output's Unit

0.0574580556193978 --> No Conversion Required

FINAL ANSWER

0.0574580556193978 ≈ 0.057458 <-- Thermal Efficiency

(Calculation completed in 00.020 seconds)

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Created by Chilvera Bhanu Teja

Institute of Aeronautical Engineering (IARE), Hyderabad

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Dayananda Sagar College of Engineering (DSCE), Bengaluru

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Thermal Efficiency of Propeller Engines

LaTeX Go Thermal Efficiency = Break Power/(Fuel Flow Rate*Fuel Calorific Value)

Propeller efficiency given thrust

LaTeX Go Propeller Efficiency = (Propeller Thrust*Flight Speed)/Shaft Power

Propeller Efficiency

LaTeX Go Propeller Efficiency = Thrust Power/Shaft Power

Total thrust given nozzle thrust and propeller thrust

LaTeX Go Total Thrust = Nozzle Thrust+Propeller Thrust

Thermal Efficiency of Propeller Engines Formula

LaTeX Go

Thermal Efficiency = Break Power/(Fuel Flow Rate*Fuel Calorific Value)
η_th = BP/(m_f*Q)

What is thermal efficiency?

Thermal efficiency is a dimensionless performance measure of a device that uses thermal energy, such as an internal combustion engine, a steam turbine or a steam engine, a boiler, furnace.

How to Calculate Thermal Efficiency of Propeller Engines?

Thermal Efficiency of Propeller Engines calculator uses Thermal Efficiency = Break Power/(Fuel Flow Rate*Fuel Calorific Value) to calculate the Thermal Efficiency, The Thermal efficiency of propeller engines formula is defined as the ratio of break power to the product of fuel flow rate and calorific value of fuel. Thermal Efficiency is denoted by η_th symbol.

How to calculate Thermal Efficiency of Propeller Engines using this online calculator? To use this online calculator for Thermal Efficiency of Propeller Engines, enter Break Power (BP), Fuel Flow Rate (m_f) & Fuel Calorific Value (Q) and hit the calculate button. Here is how the Thermal Efficiency of Propeller Engines calculation can be explained with given input values -> 0.002394 = 125000/(fuel_flow_rate*43510000).

FAQ

What is Thermal Efficiency of Propeller Engines?

The Thermal efficiency of propeller engines formula is defined as the ratio of break power to the product of fuel flow rate and calorific value of fuel and is represented as η_th = BP/(m_f*Q) or Thermal Efficiency = Break Power/(Fuel Flow Rate*Fuel Calorific Value). Break power is power developed at the output shaft, Fuel Flow Rate is the fuel mass flow rate & Fuel Calorific Value denotes the amount of heat energy released per unit mass of fuel upon complete combustion.

How to calculate Thermal Efficiency of Propeller Engines?

The Thermal efficiency of propeller engines formula is defined as the ratio of break power to the product of fuel flow rate and calorific value of fuel is calculated using Thermal Efficiency = Break Power/(Fuel Flow Rate*Fuel Calorific Value). To calculate Thermal Efficiency of Propeller Engines, you need Break Power (BP), Fuel Flow Rate (m_f) & Fuel Calorific Value (Q). With our tool, you need to enter the respective value for Break Power, Fuel Flow Rate & Fuel Calorific Value and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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