Ram Drag of Turbojet given Gross Thrust Solution

STEP 0: Pre-Calculation Summary
Formula Used
Ram Drag of Turbojet = Gross Thrust of Turbojet-Net Thrust of Turbojet
Dram = TG-T
This formula uses 3 Variables
Variables Used
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.
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.
STEP 1: Convert Input(s) to Base Unit
Gross Thrust of Turbojet: 1124 Newton --> 1124 Newton No Conversion Required
Net Thrust of Turbojet: 469 Newton --> 469 Newton No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Dram = TG-T --> 1124-469
Evaluating ... ...
Dram = 655
STEP 3: Convert Result to Output's Unit
655 Newton --> No Conversion Required
FINAL ANSWER
655 Newton <-- Ram Drag of Turbojet
(Calculation completed in 00.004 seconds)

Credits

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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!
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Verified by Kartikay Pandit
National Institute Of Technology (NIT), Hamirpur
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Ram Drag of Turbojet given Gross Thrust Formula

​LaTeX ​Go
Ram Drag of Turbojet = Gross Thrust of Turbojet-Net Thrust of Turbojet
Dram = TG-T

What is ram drag?

The loss of thrust in a turbofan or turbojet engine that is caused by increasing the velocity of the air entering the engine

How to Calculate Ram Drag of Turbojet given Gross Thrust?

Ram Drag of Turbojet given Gross Thrust calculator uses Ram Drag of Turbojet = Gross Thrust of Turbojet-Net Thrust of Turbojet to calculate the Ram Drag of Turbojet, Ram Drag of Turbojet given Gross Thrust formula is defined as the loss of thrust produced by a turbojet or turbofan engine caused by the increase of velocity of air entering the engine. Ram drag is the difference between gross thrust and net thrust. Ram Drag of Turbojet is denoted by Dram symbol.

How to calculate Ram Drag of Turbojet given Gross Thrust using this online calculator? To use this online calculator for Ram Drag of Turbojet given Gross Thrust, enter Gross Thrust of Turbojet (TG) & Net Thrust of Turbojet (T) and hit the calculate button. Here is how the Ram Drag of Turbojet given Gross Thrust calculation can be explained with given input values -> 694 = 1124-469.

FAQ

What is Ram Drag of Turbojet given Gross Thrust?
Ram Drag of Turbojet given Gross Thrust formula is defined as the loss of thrust produced by a turbojet or turbofan engine caused by the increase of velocity of air entering the engine. Ram drag is the difference between gross thrust and net thrust and is represented as Dram = TG-T or Ram Drag of Turbojet = Gross Thrust of Turbojet-Net Thrust of Turbojet. Gross Thrust of Turbojet is the total thrust force produced by a turbojet excluding the ram drag & Net Thrust of Turbojet denotes the total thrust or forward force exerted by the engine to propel an aircraft forward.
How to calculate Ram Drag of Turbojet given Gross Thrust?
Ram Drag of Turbojet given Gross Thrust formula is defined as the loss of thrust produced by a turbojet or turbofan engine caused by the increase of velocity of air entering the engine. Ram drag is the difference between gross thrust and net thrust is calculated using Ram Drag of Turbojet = Gross Thrust of Turbojet-Net Thrust of Turbojet. To calculate Ram Drag of Turbojet given Gross Thrust, you need Gross Thrust of Turbojet (TG) & Net Thrust of Turbojet (T). With our tool, you need to enter the respective value for Gross Thrust of Turbojet & Net Thrust of Turbojet 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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