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Zero-Lift Drag Coefficient given required Thrust Formula

GoZero-Lift Drag Coefficient for given Lift Coefficient Formula

GoZero-Lift Drag Coefficient for Minimum Power required 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{T}{P dynamic \cdot S}) - C D,i

C_D,0 - Zero Lift Drag Coefficient?T - Thrust?P_dynamic - Dynamic Pressure?S - Reference Area?C_D,i - Coefficient Of Drag Due to Lift?

Zero-Lift Drag Coefficient given required Thrust Example

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Here is how the Zero-Lift Drag Coefficient given required Thrust equation looks like with Values.

Here is how the Zero-Lift Drag Coefficient given required Thrust equation looks like with Units.

Here is how the Zero-Lift Drag Coefficient given required Thrust equation looks like.

0.32 = (\frac{100}{10 \cdot 8}) - 0.93

0.32 = (\frac{100N}{10Pa \cdot 8m²}) - 0.93

0.32 = (\frac{100}{10 \cdot 8}) - 0.93

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Zero-Lift Drag Coefficient given required Thrust Solution

Follow our step by step solution on how to calculate Zero-Lift Drag Coefficient given required Thrust?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

C D,0 = (\frac{100N}{10Pa \cdot 8m²}) - 0.93

Next Step Prepare to Evaluate

∴

C D,0 = (\frac{100}{10 \cdot 8}) - 0.93

LAST Step Evaluate

∴

C D,0 = 0.32

Zero-Lift Drag Coefficient given required Thrust 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

Thrust

The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air.

Symbol: T

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Thrust

Dynamic Pressure

Dynamic Pressure is a measure of the kinetic energy per unit volume of a fluid in motion.

Symbol: P_dynamic

Measurement: PressureUnit: Pa

Note: Value should be greater than 0.

Formulas to find Dynamic Pressure

Reference Area

The Reference Area is arbitrarily an area that is characteristic of the object being considered. For an aircraft wing, the wing's platform area is called the reference wing area or simply wing area.

Symbol: S

Measurement: AreaUnit: m²

Note: Value should be greater than 0.

Formulas to find Reference Area

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 for given Lift Coefficient

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

Go Zero-Lift Drag Coefficient for Minimum Power required

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

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 given required Thrust?

Zero-Lift Drag Coefficient given required Thrust evaluator uses Zero Lift Drag Coefficient = (Thrust/(Dynamic Pressure*Reference Area))-Coefficient Of Drag Due to Lift to evaluate the Zero Lift Drag Coefficient, The Zero-Lift Drag Coefficient given required Thrust is a measure of the drag experienced by an aircraft when it's not producing any lift, often during cruising or gliding, it's an essential parameter in aerodynamics, describing the inherent drag characteristics of an aircraft, including factors such as its shape, surface texture, and overall design. Zero Lift Drag Coefficient is denoted by C_D,0 symbol.

How to evaluate Zero-Lift Drag Coefficient given required Thrust using this online evaluator? To use this online evaluator for Zero-Lift Drag Coefficient given required Thrust, enter Thrust (T), Dynamic Pressure (P_dynamic), Reference Area (S) & Coefficient Of Drag Due to Lift (C_D,i) and hit the calculate button.

FAQs on Zero-Lift Drag Coefficient given required Thrust

What is the formula to find Zero-Lift Drag Coefficient given required Thrust?

The formula of Zero-Lift Drag Coefficient given required Thrust is expressed as Zero Lift Drag Coefficient = (Thrust/(Dynamic Pressure*Reference Area))-Coefficient Of Drag Due to Lift. Here is an example- 0.686 = (100/(10*8))-0.93.

How to calculate Zero-Lift Drag Coefficient given required Thrust?

With Thrust (T), Dynamic Pressure (P_dynamic), Reference Area (S) & Coefficient Of Drag Due to Lift (C_D,i) we can find Zero-Lift Drag Coefficient given required Thrust using the formula - Zero Lift Drag Coefficient = (Thrust/(Dynamic Pressure*Reference Area))-Coefficient Of Drag Due to Lift.

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*Area))-((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))
Zero Lift Drag Coefficient=Coefficient Of Drag Due to Lift/3

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Zero-Lift Drag Coefficient given required Thrust Formula

​GoZero-Lift Drag Coefficient for given Lift Coefficient Formula

​GoZero-Lift Drag Coefficient for Minimum Power required Formula

Zero-Lift Drag Coefficient given required Thrust Example

Zero-Lift Drag Coefficient given required Thrust Solution

Zero-Lift Drag Coefficient given required Thrust Formula Elements

Other Formulas to find Zero Lift Drag Coefficient

Other formulas in Lift and Drag Requirements category

How to Evaluate Zero-Lift Drag Coefficient given required Thrust?

FAQs on Zero-Lift Drag Coefficient given required Thrust

Variable Name

GoZero-Lift Drag Coefficient for given Lift Coefficient Formula

GoZero-Lift Drag Coefficient for Minimum Power required Formula