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Coefficient of drag given drag Formula

GoDrag Coefficient for given parasite drag coefficient Formula

GoDrag Coefficient for given zero-lift drag coefficient Formula

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Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water. Check FAQs

C D = \frac{C L \cdot F D}{W 0}

C_D - Drag Coefficient?C_L - Lift Coefficient?F_D - Drag Force?W₀ - Gross Weight?

Coefficient of drag given drag Example

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Here is how the Coefficient of drag given drag equation looks like with Values.

Here is how the Coefficient of drag given drag equation looks like with Units.

Here is how the Coefficient of drag given drag equation looks like.

30.0341 = \frac{1.1 \cdot 80}{2.93}

30.0341 = \frac{1.1 \cdot 80N}{2.93kg}

30.0341 = \frac{1.1 \cdot 80}{2.93}

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Coefficient of drag given drag Solution

Follow our step by step solution on how to calculate Coefficient of drag given drag?

FIRST Step Consider the formula

C D = \frac{C L \cdot F D}{W 0}

Next Step Substitute values of Variables

∴

C D = \frac{1.1 \cdot 80N}{2.93kg}

Next Step Prepare to Evaluate

∴

C D = \frac{1.1 \cdot 80}{2.93}

Next Step Evaluate

∴

C D = 30.0341296928328

LAST Step Rounding Answer

∴

C D = 30.0341

Coefficient of drag given drag Formula Elements

Variables

Drag Coefficient

Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.

Symbol: C_D

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Drag Coefficient

Lift Coefficient

The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.

Symbol: C_L

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Lift Coefficient

Drag Force

Drag Force is the resisting force experienced by an object moving through a fluid ,such as air.

Symbol: F_D

Measurement: ForceUnit: N

Note: Value can be positive or negative.

Formulas to find Drag Force

Gross Weight

The Gross Weight of the airplane is the weight with full fuel and payload.

Symbol: W₀

Measurement: WeightUnit: kg

Note: Value should be greater than 0.

Formulas to find Gross Weight

Other Formulas to find Drag Coefficient

Go Drag Coefficient for given parasite drag coefficient

C D = C D,e + (\frac{{C L}^{2}}{π \cdot e oswald \cdot AR})

Go Drag Coefficient for given zero-lift drag coefficient

C D = C D,0 + (\frac{{C L}^{2}}{π \cdot e oswald \cdot AR})

Go Drag coefficient given Drag Force

C D = \frac{F D}{q}

Go Drag coefficient given lift coefficient

C D = C L \cdot \frac{F D}{F L}

Other formulas in Lift and Drag Polar category

Go Coefficient of Drag due to lift

C D,i = \frac{{C L}^{2}}{π \cdot e oswald \cdot AR}

Go Parasite Drag Coefficient at zero lift

C D,0 = C D - C D,i

Go Modern Lift Equation

L = \frac{C L \cdot ρ air \cdot S \cdot {u f}^{2}}{2}

Go Lift coefficient given Lift Force

C L = \frac{F L}{q}

How to Evaluate Coefficient of drag given drag?

Coefficient of drag given drag evaluator uses Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight to evaluate the Drag Coefficient, Coefficient of Drag given Drag is a dimensionless quantity that represents the resistance encountered by an object moving through a fluid, calculated by dividing the drag force by the product of the lift coefficient and gross weight. Drag Coefficient is denoted by C_D symbol.

How to evaluate Coefficient of drag given drag using this online evaluator? To use this online evaluator for Coefficient of drag given drag, enter Lift Coefficient (C_L), Drag Force (F_D) & Gross Weight (W₀) and hit the calculate button.

FAQs on Coefficient of drag given drag

What is the formula to find Coefficient of drag given drag?

The formula of Coefficient of drag given drag is expressed as Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight. Here is an example- 29.93197 = (1.1*80)/2.93.

How to calculate Coefficient of drag given drag?

With Lift Coefficient (C_L), Drag Force (F_D) & Gross Weight (W₀) we can find Coefficient of drag given drag using the formula - Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight.

What are the other ways to Calculate Drag Coefficient?

Here are the different ways to Calculate Drag Coefficient-

Drag Coefficient=Parasite Drag coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))
Drag Coefficient=Zero-Lift Drag Coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))
Drag Coefficient=Drag Force/Dynamic Pressure

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