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Zero-Lift Drag Coefficient for Minimum Power required Formula

GoZero-Lift Drag Coefficient given required Thrust Formula

GoZero-Lift Drag Coefficient for given Lift Coefficient Formula

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Zero Lift Drag Coefficient is the coefficient of drag for an aircraft or aerodynamic body when it is producing zero lift. Check FAQs

C D,0 = \frac{C D,i}{3}

C_D,0 - Zero Lift Drag Coefficient?C_D,i - Coefficient Of Drag Due to Lift?

Zero-Lift Drag Coefficient for Minimum Power required Example

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Here is how the Zero-Lift Drag Coefficient for Minimum Power required equation looks like with Values.

Here is how the Zero-Lift Drag Coefficient for Minimum Power required equation looks like with Units.

Here is how the Zero-Lift Drag Coefficient for Minimum Power required equation looks like.

0.31 = \frac{0.93}{3}

0.31 = \frac{0.93}{3}

0.31 = \frac{0.93}{3}

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Zero-Lift Drag Coefficient for Minimum Power required Solution

Follow our step by step solution on how to calculate Zero-Lift Drag Coefficient for Minimum Power required?

FIRST Step Consider the formula

C D,0 = \frac{C D,i}{3}

Next Step Substitute values of Variables

∴

C D,0 = \frac{0.93}{3}

Next Step Prepare to Evaluate

∴

C D,0 = \frac{0.93}{3}

LAST Step Evaluate

∴

C D,0 = 0.31

Zero-Lift Drag Coefficient for Minimum Power required Formula Elements

Variables

Zero Lift Drag Coefficient

Zero Lift Drag Coefficient is the coefficient of drag for an aircraft or aerodynamic body when it is producing zero lift.

Symbol: C_D,0

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Zero Lift Drag Coefficient

Coefficient Of Drag Due to Lift

The Coefficient of Drag Due to Lift represents the contribution of lift-induced drag to the total drag experienced by an aircraft.

Symbol: C_D,i

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Coefficient Of Drag Due to Lift

Other Formulas to find Zero Lift Drag Coefficient

Go Zero-Lift Drag Coefficient given required Thrust

C D,0 = (\frac{T}{P dynamic \cdot S}) - C D,i

Go Zero-Lift Drag Coefficient for given Lift Coefficient

C D,0 = (\frac{T}{P dynamic \cdot A}) - (\frac{{C L}^{2}}{π \cdot e \cdot AR})

Other formulas in Lift and Drag Requirements category

Go Drag for Level and Unaccelerated Flight

F D = T \cdot \cos (σ T)

Go Lift for Unaccelerated Flight

F L = W body - T \cdot \sin (σ T)

Go Drag for Level and Unaccelerated Flight at Negligible Thrust Angle

F D = P dynamic \cdot A \cdot C D

Go Lift for Level and Unaccelerated Flight at Negligible Thrust Angle

F L = P dynamic \cdot A \cdot C L

How to Evaluate Zero-Lift Drag Coefficient for Minimum Power required?

Zero-Lift Drag Coefficient for Minimum Power required evaluator uses Zero Lift Drag Coefficient = Coefficient Of Drag Due to Lift/3 to evaluate the Zero Lift Drag Coefficient, The Zero-Lift Drag Coefficient for Minimum Power required typically represents the baseline drag of the aircraft, excluding the effects of lift, therefore, it's often associated with the minimum drag configuration and consequently the minimum power required for level flight. Zero Lift Drag Coefficient is denoted by C_D,0 symbol.

How to evaluate Zero-Lift Drag Coefficient for Minimum Power required using this online evaluator? To use this online evaluator for Zero-Lift Drag Coefficient for Minimum Power required, enter Coefficient Of Drag Due to Lift (C_D,i) and hit the calculate button.

FAQs on Zero-Lift Drag Coefficient for Minimum Power required

What is the formula to find Zero-Lift Drag Coefficient for Minimum Power required?

The formula of Zero-Lift Drag Coefficient for Minimum Power required is expressed as Zero Lift Drag Coefficient = Coefficient Of Drag Due to Lift/3. Here is an example- 0.188 = 0.93/3.

How to calculate Zero-Lift Drag Coefficient for Minimum Power required?

With Coefficient Of Drag Due to Lift (C_D,i) we can find Zero-Lift Drag Coefficient for Minimum Power required using the formula - Zero Lift Drag Coefficient = Coefficient Of Drag Due to Lift/3.

What are the other ways to Calculate Zero Lift Drag Coefficient?

Here are the different ways to Calculate Zero Lift Drag Coefficient-

Zero Lift Drag Coefficient=(Thrust/(Dynamic Pressure*Reference Area))-Coefficient Of Drag Due to Lift
Zero Lift Drag Coefficient=(Thrust/(Dynamic Pressure*Area))-((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))

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