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Gross Thrust Coefficient Formula

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Gross Thrust Coefficient is the ratio of actual gross thrust to the ideal gross thrust. Check FAQs

C Tg = \frac{T G}{F i}

C_Tg - Gross Thrust Coefficient?T_G - Gross Thrust?F_i - Ideal Gross Thrust?

Gross Thrust Coefficient Example

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Here is how the Gross Thrust Coefficient equation looks like with Values.

Here is how the Gross Thrust Coefficient equation looks like with Units.

Here is how the Gross Thrust Coefficient equation looks like.

0.8189 = \frac{868}{1060}

0.8189 = \frac{868N}{1060N}

0.8189 = \frac{868}{1060}

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Gross Thrust Coefficient Solution

Follow our step by step solution on how to calculate Gross Thrust Coefficient?

FIRST Step Consider the formula

C Tg = \frac{T G}{F i}

Next Step Substitute values of Variables

∴

C Tg = \frac{868N}{1060N}

Next Step Prepare to Evaluate

∴

C Tg = \frac{868}{1060}

Next Step Evaluate

∴

C Tg = 0.818867924528302

LAST Step Rounding Answer

∴

C Tg = 0.8189

Gross Thrust Coefficient Formula Elements

Variables

Gross Thrust Coefficient

Gross Thrust Coefficient is the ratio of actual gross thrust to the ideal gross thrust.

Symbol: C_Tg

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Gross Thrust Coefficient

Gross Thrust

Gross Thrust is the total thrust of a jet engine without deduction of the drag caused by the momentum of the incoming air.

Symbol: T_G

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Gross Thrust

Ideal Gross Thrust

Ideal Gross Thrust is thrust without losses.

Symbol: F_i

Measurement: ForceUnit: N

Note: Value can be positive or negative.

Formulas to find Ideal Gross Thrust

Other formulas in Thrust Generation category

Go Total Thrust given Efficiency and Enthalpy

T total = m a \cdot ((\sqrt{2 \cdot Δh nozzle \cdot η nozzle}) - V + (\sqrt{η T \cdot η transmission \cdot Δh turbine}))

Go Ideal Thrust given Effective Speed Ratio

T ideal = m a \cdot V \cdot ((\frac{1}{α}) - 1)

Go Thrust power

T P = m a \cdot V \cdot (V e - V)

Go Specific thrust

I sp = V e - V

How to Evaluate Gross Thrust Coefficient?

Gross Thrust Coefficient evaluator uses Gross Thrust Coefficient = Gross Thrust/Ideal Gross Thrust to evaluate the Gross Thrust Coefficient, Gross Thrust Coefficient is a dimensionless measure of the efficiency of an aircraft engine or rocket, calculated as the ratio of gross thrust to ideal gross thrust, providing a comparative assessment of an engine's performance under varying conditions. Gross Thrust Coefficient is denoted by C_Tg symbol.

How to evaluate Gross Thrust Coefficient using this online evaluator? To use this online evaluator for Gross Thrust Coefficient, enter Gross Thrust (T_G) & Ideal Gross Thrust (F_i) and hit the calculate button.

FAQs on Gross Thrust Coefficient

What is the formula to find Gross Thrust Coefficient?

The formula of Gross Thrust Coefficient is expressed as Gross Thrust Coefficient = Gross Thrust/Ideal Gross Thrust. Here is an example- 7 = 868/ideal_gross_thrust.

How to calculate Gross Thrust Coefficient?

With Gross Thrust (T_G) & Ideal Gross Thrust (F_i) we can find Gross Thrust Coefficient using the formula - Gross Thrust Coefficient = Gross Thrust/Ideal Gross Thrust.

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