Gross Thrust of Turbojet given Net Thrust Calculator

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

✖Gross Thrust of Turbojet is the total thrust force produced by a turbojet excluding the ram drag.ⓘ Gross Thrust of Turbojet given Net Thrust [T_G]

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Gross Thrust of Turbojet given Net Thrust Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

Variables Used

Gross Thrust of Turbojet - (Measured in Newton) - Gross Thrust of Turbojet is the total thrust force produced by a turbojet excluding the ram drag.
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.
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

Net Thrust of Turbojet: 469 Newton --> 469 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_G = T+D_ram --> 469+655

Evaluating ... ...

T_G = 1124

STEP 3: Convert Result to Output's Unit

1124 Newton --> No Conversion Required

FINAL ANSWER

1124 Newton <-- Gross Thrust of Turbojet

(Calculation completed in 00.004 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

Gross Thrust of Turbojet given Net Thrust Formula

LaTeX Go

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

What is gross thrust?

Gross or total thrust is the product of the mass of air passing through the engine and the jet velocity at the propelling nozzle.

How to Calculate Gross Thrust of Turbojet given Net Thrust?

Gross Thrust of Turbojet given Net Thrust calculator uses Gross Thrust of Turbojet = Net Thrust of Turbojet+Ram Drag of Turbojet to calculate the Gross Thrust of Turbojet, Gross Thrust of Turbojet given Net Thrust is a measure of the total forward force exerted by a turbojet engine, representing the combination of the net thrust produced by the engine and the ram drag caused by the inward motion of air. Gross Thrust of Turbojet is denoted by T_G symbol.

How to calculate Gross Thrust of Turbojet given Net Thrust using this online calculator? To use this online calculator for Gross Thrust of Turbojet given Net Thrust, enter Net Thrust of Turbojet (T) & Ram Drag of Turbojet (D_ram) and hit the calculate button. Here is how the Gross Thrust of Turbojet given Net Thrust calculation can be explained with given input values -> 1124 = 469+655.

FAQ

What is Gross Thrust of Turbojet given Net Thrust?

Gross Thrust of Turbojet given Net Thrust is a measure of the total forward force exerted by a turbojet engine, representing the combination of the net thrust produced by the engine and the ram drag caused by the inward motion of air and is represented as T_G = T+D_ram or Gross Thrust of Turbojet = Net Thrust of Turbojet+Ram Drag of Turbojet. Net Thrust of Turbojet denotes the total thrust or forward force exerted by the engine to propel an aircraft forward & 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 Gross Thrust of Turbojet given Net Thrust?

Gross Thrust of Turbojet given Net Thrust is a measure of the total forward force exerted by a turbojet engine, representing the combination of the net thrust produced by the engine and the ram drag caused by the inward motion of air is calculated using Gross Thrust of Turbojet = Net Thrust of Turbojet+Ram Drag of Turbojet. To calculate Gross Thrust of Turbojet given Net Thrust, you need Net Thrust of Turbojet (T) & Ram Drag of Turbojet (D_ram). With our tool, you need to enter the respective value for Net 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 Gross Thrust of Turbojet?

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

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

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