Gross Thrust of Turbojet given Net Thrust Calculator

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✖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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Formula

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Gross Thrust of Turbojet given Net Thrust

Formula

`"T"_{"G"} = "T"+"D"_{"ram"}`

Example

`"1124N"="469N"+"655N"`

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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

Himanshu Sharma has created this Calculator and 50+ more calculators!

Verified by Kartikay Pandit

National Institute Of Technology (NIT), Hamirpur

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< 14 Turbojets Calculators

Mass Flow Rate in Turbojet given Thrust

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

Exhaust Velocity given Thrust in Turbojet

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

Flight Speed given Thrust in Turbojet

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

Nozzle Exit Area in Turbojet

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)

Net Thrust Produced by Turbojet

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

Exhaust Velocity given Gross Thrust in Turbojet

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

Mass Flow Rate of Turbojet given Gross Thrust

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

Turbojet Gross Thrust

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

Thermal efficiency of turbojet engine

Go Turbojet Thermal Efficiency = Propulsive Power/(Fuel Flow Rate*Fuel Calorific Value)

Net Thrust of Turbojet given Gross Thrust

Go Net Thrust of Turbojet = Gross Thrust of Turbojet-Ram Drag of Turbojet

Gross Thrust of Turbojet given Net Thrust

Go Gross Thrust of Turbojet = Net Thrust of Turbojet+Ram Drag of Turbojet

Ram Drag of Turbojet given Gross Thrust

Go Ram Drag of Turbojet = Gross Thrust of Turbojet-Net Thrust of Turbojet

Mass Flow Rate of Exhaust Gases

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

Mass Flow Rate of Exhaust Gases given Fuel Air Ratio

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

Gross Thrust of Turbojet given Net Thrust Formula

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 formula is defined as the sum of the net produced thrust of the turbojet and the momentum drag of the thrust. 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 formula is defined as the sum of the net produced thrust of the turbojet and the momentum drag of the thrust 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 formula is defined as the sum of the net produced thrust of the turbojet and the momentum drag of the thrust 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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