Net Thrust of Turbojet given Gross Thrust Calculator

✖Gross Thrust of Turbojet is the total thrust force produced by a turbojet excluding the ram drag.ⓘ Gross Thrust of Turbojet [T_G]			+10% -10%
✖Ram Drag of Turbojet refers to the drag force experienced by a turbojet engine due to the impact of air at high speeds.ⓘ Ram Drag of Turbojet [D_ram]			+10% -10%

✖Net Thrust of Turbojet denotes the total thrust or forward force exerted by the engine to propel an aircraft forward.ⓘ Net Thrust of Turbojet given Gross Thrust [T]

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Net Thrust of Turbojet given Gross Thrust Solution

STEP 0: Pre-Calculation Summary

Formula Used

Net Thrust of Turbojet = Gross Thrust of Turbojet-Ram Drag of Turbojet
T = T_G-D_ram
This formula uses 3 Variables

Variables Used

Net Thrust of Turbojet - (Measured in Newton) - Net Thrust of Turbojet denotes the total thrust or forward force exerted by the engine to propel an aircraft forward.
Gross Thrust of Turbojet - (Measured in Newton) - Gross Thrust of Turbojet is the total thrust force produced by a turbojet excluding the ram drag.
Ram Drag of Turbojet - (Measured in Newton) - Ram Drag of Turbojet refers to the drag force experienced by a turbojet engine due to the impact of air at high speeds.

STEP 1: Convert Input(s) to Base Unit

Gross Thrust of Turbojet: 1124 Newton --> 1124 Newton No Conversion Required
Ram Drag of Turbojet: 655 Newton --> 655 Newton No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

T = T_G-D_ram --> 1124-655

Evaluating ... ...

T = 469

STEP 3: Convert Result to Output's Unit

469 Newton --> No Conversion Required

FINAL ANSWER

469 Newton <-- Net Thrust of Turbojet

(Calculation completed in 00.007 seconds)

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Created by Himanshu Sharma

National Institute of Technology, Hamirpur (NITH), Himachal Pradesh

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National Institute Of Technology (NIT), Hamirpur

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< Turbojets Calculators

Nozzle Exit Area in Turbojet

LaTeX Go Nozzle Exit Area = (Net Thrust of Turbojet-Mass Flow Rate Turbojet*(1+Fuel Air Ratio)*(Exit Velocity-Flight Speed))/(Nozzle Exit Pressure-Ambient Pressure)

Turbojet Gross Thrust

LaTeX Go Gross Thrust of Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio)*Exit Velocity+(Nozzle Exit Pressure-Ambient Pressure)*Nozzle Exit Area

Mass Flow Rate of Exhaust Gases given Fuel Air Ratio

LaTeX Go Total Mass Flow Rate Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio)

Mass Flow Rate of Exhaust Gases

LaTeX Go Total Mass Flow Rate Turbojet = Mass Flow Rate Turbojet+Fuel Flow Rate

Net Thrust of Turbojet given Gross Thrust Formula

LaTeX Go

Net Thrust of Turbojet = Gross Thrust of Turbojet-Ram Drag of Turbojet
T = T_G-D_ram

What is net thrust?

The thrust produced by a turbojet engine in flight. The net thrust or resultant force acting on the aircraft in flight is the difference between the gross thrust and the momentum drag.

How to Calculate Net Thrust of Turbojet given Gross Thrust?

Net Thrust of Turbojet given Gross Thrust calculator uses Net Thrust of Turbojet = Gross Thrust of Turbojet-Ram Drag of Turbojet to calculate the Net Thrust of Turbojet, Net Thrust of Turbojet given Gross Thrust is a measure of the forward force exerted by a turbojet engine, calculated by subtracting the ram drag from the gross thrust, providing insight into the engine's overall performance and efficiency. Net Thrust of Turbojet is denoted by T symbol.

How to calculate Net Thrust of Turbojet given Gross Thrust using this online calculator? To use this online calculator for Net Thrust of Turbojet given Gross Thrust, enter Gross Thrust of Turbojet (T_G) & Ram Drag of Turbojet (D_ram) and hit the calculate button. Here is how the Net Thrust of Turbojet given Gross Thrust calculation can be explained with given input values -> 508 = 1124-655.

FAQ

What is Net Thrust of Turbojet given Gross Thrust?

Net Thrust of Turbojet given Gross Thrust is a measure of the forward force exerted by a turbojet engine, calculated by subtracting the ram drag from the gross thrust, providing insight into the engine's overall performance and efficiency and is represented as T = T_G-D_ram or Net Thrust of Turbojet = Gross Thrust of Turbojet-Ram Drag of Turbojet. Gross Thrust of Turbojet is the total thrust force produced by a turbojet excluding the ram drag & Ram Drag of Turbojet refers to the drag force experienced by a turbojet engine due to the impact of air at high speeds.

How to calculate Net Thrust of Turbojet given Gross Thrust?

Net Thrust of Turbojet given Gross Thrust is a measure of the forward force exerted by a turbojet engine, calculated by subtracting the ram drag from the gross thrust, providing insight into the engine's overall performance and efficiency is calculated using Net Thrust of Turbojet = Gross Thrust of Turbojet-Ram Drag of Turbojet. To calculate Net Thrust of Turbojet given Gross Thrust, you need Gross Thrust of Turbojet (T_G) & Ram Drag of Turbojet (D_ram). With our tool, you need to enter the respective value for Gross Thrust of Turbojet & Ram Drag of Turbojet 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 Net Thrust of Turbojet?

In this formula, Net Thrust of Turbojet uses Gross Thrust of Turbojet & Ram Drag of Turbojet. We can use 1 other way(s) to calculate the same, which is/are as follows -

Net Thrust of Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio)*(Exit Velocity-Flight Speed)+Nozzle Exit Area*(Nozzle Exit Pressure-Ambient Pressure)

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