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Coefficient of Drag for given Thrust and Weight Formula

GoCoefficient of Drag for given Thrust-to-Weight Ratio 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{T \cdot C L}{W body}

C_D - Drag Coefficient?T - Thrust?C_L - Lift Coefficient?W_body - Weight of Body?

Coefficient of Drag for given Thrust and Weight Example

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Here is how the Coefficient of Drag for given Thrust and Weight equation looks like with Values.

Here is how the Coefficient of Drag for given Thrust and Weight equation looks like with Units.

Here is how the Coefficient of Drag for given Thrust and Weight equation looks like.

0.4977 = \frac{100 \cdot 1.1}{221}

0.4977 = \frac{100N \cdot 1.1}{221N}

0.4977 = \frac{100 \cdot 1.1}{221}

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Coefficient of Drag for given Thrust and Weight Solution

Follow our step by step solution on how to calculate Coefficient of Drag for given Thrust and Weight?

FIRST Step Consider the formula

C D = \frac{T \cdot C L}{W body}

Next Step Substitute values of Variables

∴

C D = \frac{100N \cdot 1.1}{221N}

Next Step Prepare to Evaluate

∴

C D = \frac{100 \cdot 1.1}{221}

Next Step Evaluate

∴

C D = 0.497737556561086

LAST Step Rounding Answer

∴

C D = 0.4977

Coefficient of Drag for given Thrust and Weight 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

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

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

Weight of Body

Weight of Body is the force acting on the object due to gravity.

Symbol: W_body

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Weight of Body

Other Formulas to find Drag Coefficient

Go Coefficient of Drag for given Thrust-to-Weight Ratio

C D = C L \cdot TW

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 Coefficient of Drag for given Thrust and Weight?

Coefficient of Drag for given Thrust and Weight evaluator uses Drag Coefficient = (Thrust*Lift Coefficient)/Weight of Body to evaluate the Drag Coefficient, The Coefficient of Drag for given thrust and weight is a dimensionless quantity that represents the aerodynamic drag experienced by an object moving through a fluid, it quantifies the resistance encountered by the object due to factors such as friction and pressure, this equation suggests that the drag coefficient can be determined based on the thrust generated by the propulsion system, the lift coefficient representing the aerodynamic lift, and the weight of the object. Drag Coefficient is denoted by C_D symbol.

How to evaluate Coefficient of Drag for given Thrust and Weight using this online evaluator? To use this online evaluator for Coefficient of Drag for given Thrust and Weight, enter Thrust (T), Lift Coefficient (C_L) & Weight of Body (W_body) and hit the calculate button.

FAQs on Coefficient of Drag for given Thrust and Weight

What is the formula to find Coefficient of Drag for given Thrust and Weight?

The formula of Coefficient of Drag for given Thrust and Weight is expressed as Drag Coefficient = (Thrust*Lift Coefficient)/Weight of Body. Here is an example- 0.497738 = (100*1.1)/221.

How to calculate Coefficient of Drag for given Thrust and Weight?

With Thrust (T), Lift Coefficient (C_L) & Weight of Body (W_body) we can find Coefficient of Drag for given Thrust and Weight using the formula - Drag Coefficient = (Thrust*Lift Coefficient)/Weight of Body.

What are the other ways to Calculate Drag Coefficient?

Here are the different ways to Calculate Drag Coefficient-

Drag Coefficient=Lift Coefficient*Thrust-to-Weight Ratio

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Coefficient of Drag for given Thrust and Weight Formula

​GoCoefficient of Drag for given Thrust-to-Weight Ratio Formula

Coefficient of Drag for given Thrust and Weight Example

Coefficient of Drag for given Thrust and Weight Solution

Coefficient of Drag for given Thrust and Weight Formula Elements

Other Formulas to find Drag Coefficient

Other formulas in Lift and Drag Requirements category

How to Evaluate Coefficient of Drag for given Thrust and Weight?

FAQs on Coefficient of Drag for given Thrust and Weight

Variable Name

GoCoefficient of Drag for given Thrust-to-Weight Ratio Formula