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Drag coefficient given Drag Force 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{F D}{q}

C_D - Drag Coefficient?F_D - Drag Force?q - Dynamic Pressure?

Drag coefficient given Drag Force Example

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Here is how the Drag coefficient given Drag Force equation looks like with Values.

Here is how the Drag coefficient given Drag Force equation looks like with Units.

Here is how the Drag coefficient given Drag Force equation looks like.

29.9963 = \frac{80}{2.667}

29.9963 = \frac{80N}{2.667Pa}

29.9963 = \frac{80}{2.667}

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Drag coefficient given Drag Force Solution

Follow our step by step solution on how to calculate Drag coefficient given Drag Force?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

C D = \frac{80N}{2.667Pa}

Next Step Prepare to Evaluate

∴

C D = \frac{80}{2.667}

Next Step Evaluate

∴

C D = 29.9962504686914

LAST Step Rounding Answer

∴

C D = 29.9963

Drag coefficient given Drag Force 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

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

Dynamic Pressure

Dynamic pressure, also referred to as velocity pressure, is a specific type of pressure associated with the kinetic energy per unit volume of a moving fluid.

Symbol: q

Measurement: PressureUnit: Pa

Note: Value should be greater than 0.

Formulas to find Dynamic Pressure

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 Coefficient of drag given drag

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

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 Drag coefficient given Drag Force?

Drag coefficient given Drag Force evaluator uses Drag Coefficient = Drag Force/Dynamic Pressure to evaluate the Drag Coefficient, Drag coefficient given Drag Force represents a dimensionless quantity that represents the resistance to motion of an object through a fluid, such as air or water, and is calculated as the ratio of the drag force to the dynamic pressure. Drag Coefficient is denoted by C_D symbol.

How to evaluate Drag coefficient given Drag Force using this online evaluator? To use this online evaluator for Drag coefficient given Drag Force, enter Drag Force (F_D) & Dynamic Pressure (q) and hit the calculate button.

FAQs on Drag coefficient given Drag Force

What is the formula to find Drag coefficient given Drag Force?

The formula of Drag coefficient given Drag Force is expressed as Drag Coefficient = Drag Force/Dynamic Pressure. Here is an example- 30.07519 = 80/2.667.

How to calculate Drag coefficient given Drag Force?

With Drag Force (F_D) & Dynamic Pressure (q) we can find Drag coefficient given Drag Force using the formula - Drag Coefficient = Drag Force/Dynamic Pressure.

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=(Lift Coefficient*Drag Force)/Gross Weight

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