Ram Drag of Turbojet given Gross Thrust Formula

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Ram Drag of Turbojet refers to the drag force experienced by a turbojet engine due to the impact of air at high speeds. Check FAQs
Dram=TG-T
Dram - Ram Drag of Turbojet?TG - Gross Thrust of Turbojet?T - Net Thrust of Turbojet?

Ram Drag of Turbojet given Gross Thrust Example

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With units
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Here is how the Ram Drag of Turbojet given Gross Thrust equation looks like with Values.

Here is how the Ram Drag of Turbojet given Gross Thrust equation looks like with Units.

Here is how the Ram Drag of Turbojet given Gross Thrust equation looks like.

655Edit=1124Edit-469Edit
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Ram Drag of Turbojet given Gross Thrust Solution

Follow our step by step solution on how to calculate Ram Drag of Turbojet given Gross Thrust?

FIRST Step Consider the formula
Dram=TG-T
Next Step Substitute values of Variables
Dram=1124N-469N
Next Step Prepare to Evaluate
Dram=1124-469
LAST Step Evaluate
Dram=655N

Ram Drag of Turbojet given Gross Thrust Formula Elements

Variables
Ram Drag of Turbojet
Ram Drag of Turbojet refers to the drag force experienced by a turbojet engine due to the impact of air at high speeds.
Symbol: Dram
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Gross Thrust of Turbojet
Gross Thrust of Turbojet is the total thrust force produced by a turbojet excluding the ram drag.
Symbol: TG
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Net Thrust of Turbojet
Net Thrust of Turbojet denotes the total thrust or forward force exerted by the engine to propel an aircraft forward.
Symbol: T
Measurement: ForceUnit: N
Note: Value should be greater than 0.

Other formulas in Turbojets category

​Go Mass Flow Rate of Exhaust Gases
mtotal=ma+mf
​Go Mass Flow Rate of Exhaust Gases given Fuel Air Ratio
mtotal=ma(1+f)
​Go Turbojet Gross Thrust
TG=ma(1+f)Ve+(pe-p)Ae
​Go Nozzle Exit Area in Turbojet
Ae=T-ma(1+f)(Ve-V)pe-p

How to Evaluate Ram Drag of Turbojet given Gross Thrust?

Ram Drag of Turbojet given Gross Thrust evaluator uses Ram Drag of Turbojet = Gross Thrust of Turbojet-Net Thrust of Turbojet to evaluate 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 evaluate Ram Drag of Turbojet given Gross Thrust using this online evaluator? To use this online evaluator for Ram Drag of Turbojet given Gross Thrust, enter Gross Thrust of Turbojet (TG) & Net Thrust of Turbojet (T) and hit the calculate button.

FAQs on Ram Drag of Turbojet given Gross Thrust

What is the formula to find Ram Drag of Turbojet given Gross Thrust?
The formula of Ram Drag of Turbojet given Gross Thrust is expressed as Ram Drag of Turbojet = Gross Thrust of Turbojet-Net Thrust of Turbojet. Here is an example- 694 = 1124-469.
How to calculate Ram Drag of Turbojet given Gross Thrust?
With Gross Thrust of Turbojet (TG) & Net Thrust of Turbojet (T) we can find Ram Drag of Turbojet given Gross Thrust using the formula - Ram Drag of Turbojet = Gross Thrust of Turbojet-Net Thrust of Turbojet.
Can the Ram Drag of Turbojet given Gross Thrust be negative?
No, the Ram Drag of Turbojet given Gross Thrust, measured in Force cannot be negative.
Which unit is used to measure Ram Drag of Turbojet given Gross Thrust?
Ram Drag of Turbojet given Gross Thrust is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Ram Drag of Turbojet given Gross Thrust can be measured.
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