Total Thrust given Efficiency and Enthalpy Calculator

✖Mass Flow Rate represents the amount of mass passing through a system per unit of time.ⓘ Mass Flow Rate [m_a]			+10% -10%
✖Enthalpy Drop in Nozzle is the difference of enthalpy of inlet and exit of nozzle.ⓘ Enthalpy Drop in Nozzle [Δh_nozzle]			+10% -10%
✖Nozzle Efficiency is a measure of how effectively a nozzle converts the thermal energy of a fluid into kinetic energy.ⓘ Nozzle Efficiency [η_nozzle]			+10% -10%
✖Flight Speed refers to the velocity at which an aircraft moves through the air.ⓘ Flight Speed [V]			+10% -10%
✖Turbine Efficiency represents the ratio of the actual work output of a turbine to the maximum(isentropic) work output it could theoretically achieve.ⓘ Turbine Efficiency [η_T]			+10% -10%
✖Efficiency of Transmission is a measure of how effectively power or energy is transferred from one point to another in a system. It is the ratio of output of transmission to input of transmission.ⓘ Efficiency of Transmission [η_transmission]			+10% -10%
✖Enthalpy Drop in Turbine is the difference of enthalpy at inlet and exit of turbine.ⓘ Enthalpy Drop in Turbine [Δh_turbine]			+10% -10%

✖Total Thrust is the sum of all the thrusts produced in a system or plant.ⓘ Total Thrust given Efficiency and Enthalpy [T_total]

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Total Thrust given Efficiency and Enthalpy Solution

STEP 0: Pre-Calculation Summary

Formula Used

Total Thrust = Mass Flow Rate*((sqrt(2*Enthalpy Drop in Nozzle*Nozzle Efficiency))-Flight Speed+(sqrt(Turbine Efficiency*Efficiency of Transmission*Enthalpy Drop in Turbine)))
T_total = m_a*((sqrt(2*Δh_nozzle*η_nozzle))-V+(sqrt(η_T*η_transmission*Δh_turbine)))
This formula uses 1 Functions, 8 Variables

Functions Used

sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)

Variables Used

Total Thrust - (Measured in Newton) - Total Thrust is the sum of all the thrusts produced in a system or plant.
Mass Flow Rate - (Measured in Kilogram per Second) - Mass Flow Rate represents the amount of mass passing through a system per unit of time.
Enthalpy Drop in Nozzle - (Measured in Joule) - Enthalpy Drop in Nozzle is the difference of enthalpy of inlet and exit of nozzle.
Nozzle Efficiency - Nozzle Efficiency is a measure of how effectively a nozzle converts the thermal energy of a fluid into kinetic energy.
Flight Speed - (Measured in Meter per Second) - Flight Speed refers to the velocity at which an aircraft moves through the air.
Turbine Efficiency - Turbine Efficiency represents the ratio of the actual work output of a turbine to the maximum(isentropic) work output it could theoretically achieve.
Efficiency of Transmission - Efficiency of Transmission is a measure of how effectively power or energy is transferred from one point to another in a system. It is the ratio of output of transmission to input of transmission.
Enthalpy Drop in Turbine - (Measured in Joule) - Enthalpy Drop in Turbine is the difference of enthalpy at inlet and exit of turbine.

STEP 1: Convert Input(s) to Base Unit

Mass Flow Rate: 3.5 Kilogram per Second --> 3.5 Kilogram per Second No Conversion Required
Enthalpy Drop in Nozzle: 12 Kilojoule --> 12000 Joule (Check conversion here)
Nozzle Efficiency: 0.24 --> No Conversion Required
Flight Speed: 111 Meter per Second --> 111 Meter per Second No Conversion Required
Turbine Efficiency: 0.86 --> No Conversion Required
Efficiency of Transmission: 0.97 --> No Conversion Required
Enthalpy Drop in Turbine: 50 Kilojoule --> 50000 Joule (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

T_total = m_a*((sqrt(2*Δh_nozzle*η_nozzle))-V+(sqrt(η_T*η_transmission*Δh_turbine))) --> 3.5*((sqrt(2*12000*0.24))-111+(sqrt(0.86*0.97*50000)))

Evaluating ... ...

T_total = 591.937241168876

STEP 3: Convert Result to Output's Unit

591.937241168876 Newton --> No Conversion Required

FINAL ANSWER

591.937241168876 ≈ 591.9372 Newton <-- Total Thrust

(Calculation completed in 00.004 seconds)

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Institute of Aeronautical Engineering (IARE), Hyderabad

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< Thrust Generation Calculators

Total Thrust given Efficiency and Enthalpy

LaTeX Go Total Thrust = Mass Flow Rate*((sqrt(2*Enthalpy Drop in Nozzle*Nozzle Efficiency))-Flight Speed+(sqrt(Turbine Efficiency*Efficiency of Transmission*Enthalpy Drop in Turbine)))

Thrust power

LaTeX Go Thrust Power = Mass Flow Rate*Flight Speed*(Exit Velocity-Flight Speed)

Ideal Thrust given Effective Speed Ratio

LaTeX Go Ideal Thrust = Mass Flow Rate*Flight Speed*((1/Effective Speed Ratio)-1)

Specific thrust

LaTeX Go Specific Thrust = Exit Velocity-Flight Speed

Total Thrust given Efficiency and Enthalpy Formula

LaTeX Go

What is thrust?

Thrust is the force which moves an aircraft through the air. Thrust is used to overcome the drag of an airplane, and to overcome the weight of a rocket.

How to Calculate Total Thrust given Efficiency and Enthalpy?

Total Thrust given Efficiency and Enthalpy calculator uses Total Thrust = Mass Flow Rate*((sqrt(2*Enthalpy Drop in Nozzle*Nozzle Efficiency))-Flight Speed+(sqrt(Turbine Efficiency*Efficiency of Transmission*Enthalpy Drop in Turbine))) to calculate the Total Thrust, Total Thrust given Efficiency and Enthalpy is a measure of the total thrust generated by an aircraft engine, calculated by considering the mass flow rate, enthalpy drop in the nozzle, nozzle efficiency, flight speed, turbine efficiency, and transmission efficiency, providing a comprehensive estimate of the engine's performance. Total Thrust is denoted by T_total symbol.

How to calculate Total Thrust given Efficiency and Enthalpy using this online calculator? To use this online calculator for Total Thrust given Efficiency and Enthalpy, enter Mass Flow Rate (m_a), Enthalpy Drop in Nozzle (Δh_nozzle), Nozzle Efficiency (η_nozzle), Flight Speed (V), Turbine Efficiency (η_T), Efficiency of Transmission (η_transmission) & Enthalpy Drop in Turbine (Δh_turbine) and hit the calculate button. Here is how the Total Thrust given Efficiency and Enthalpy calculation can be explained with given input values -> 591.9372 = 3.5*((sqrt(2*12000*0.24))-111+(sqrt(0.86*0.97*50000))).

FAQ

What is Total Thrust given Efficiency and Enthalpy?

Total Thrust given Efficiency and Enthalpy is a measure of the total thrust generated by an aircraft engine, calculated by considering the mass flow rate, enthalpy drop in the nozzle, nozzle efficiency, flight speed, turbine efficiency, and transmission efficiency, providing a comprehensive estimate of the engine's performance and is represented as T_total = m_a*((sqrt(2*Δh_nozzle*η_nozzle))-V+(sqrt(η_T*η_transmission*Δh_turbine))) or Total Thrust = Mass Flow Rate*((sqrt(2*Enthalpy Drop in Nozzle*Nozzle Efficiency))-Flight Speed+(sqrt(Turbine Efficiency*Efficiency of Transmission*Enthalpy Drop in Turbine))). Mass Flow Rate represents the amount of mass passing through a system per unit of time, Enthalpy Drop in Nozzle is the difference of enthalpy of inlet and exit of nozzle, Nozzle Efficiency is a measure of how effectively a nozzle converts the thermal energy of a fluid into kinetic energy, Flight Speed refers to the velocity at which an aircraft moves through the air, Turbine Efficiency represents the ratio of the actual work output of a turbine to the maximum(isentropic) work output it could theoretically achieve, Efficiency of Transmission is a measure of how effectively power or energy is transferred from one point to another in a system. It is the ratio of output of transmission to input of transmission & Enthalpy Drop in Turbine is the difference of enthalpy at inlet and exit of turbine.

How to calculate Total Thrust given Efficiency and Enthalpy?

Total Thrust given Efficiency and Enthalpy is a measure of the total thrust generated by an aircraft engine, calculated by considering the mass flow rate, enthalpy drop in the nozzle, nozzle efficiency, flight speed, turbine efficiency, and transmission efficiency, providing a comprehensive estimate of the engine's performance is calculated using Total Thrust = Mass Flow Rate*((sqrt(2*Enthalpy Drop in Nozzle*Nozzle Efficiency))-Flight Speed+(sqrt(Turbine Efficiency*Efficiency of Transmission*Enthalpy Drop in Turbine))). To calculate Total Thrust given Efficiency and Enthalpy, you need Mass Flow Rate (m_a), Enthalpy Drop in Nozzle (Δh_nozzle), Nozzle Efficiency (η_nozzle), Flight Speed (V), Turbine Efficiency (η_T), Efficiency of Transmission (η_transmission) & Enthalpy Drop in Turbine (Δh_turbine). With our tool, you need to enter the respective value for Mass Flow Rate, Enthalpy Drop in Nozzle, Nozzle Efficiency, Flight Speed, Turbine Efficiency, Efficiency of Transmission & Enthalpy Drop in Turbine 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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