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Weight of Aircraft for given Coefficients of Lift and Drag Formula

GoWeight of Aircraft in Level, Unaccelerated Flight Formula

GoWeight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle Formula

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

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

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

Weight of Aircraft for given Coefficients of Lift and Drag Example

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Here is how the Weight of Aircraft for given Coefficients of Lift and Drag equation looks like with Values.

Here is how the Weight of Aircraft for given Coefficients of Lift and Drag equation looks like with Units.

Here is how the Weight of Aircraft for given Coefficients of Lift and Drag equation looks like.

220 = 1.1 \cdot \frac{100}{0.5}

220N = 1.1 \cdot \frac{100N}{0.5}

220 = 1.1 \cdot \frac{100}{0.5}

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Aircraft Mechanics » fx Weight of Aircraft for given Coefficients of Lift and Drag

Weight of Aircraft for given Coefficients of Lift and Drag Solution

Follow our step by step solution on how to calculate Weight of Aircraft for given Coefficients of Lift and Drag?

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

W body = 1.1 \cdot \frac{100N}{0.5}

Next Step Prepare to Evaluate

∴

W body = 1.1 \cdot \frac{100}{0.5}

LAST Step Evaluate

∴

W body = 220N

Weight of Aircraft for given Coefficients of Lift and Drag Formula Elements

Variables

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

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

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

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

Other Formulas to find Weight of Body

Go Weight of Aircraft in Level, Unaccelerated Flight

W body = F L + (T \cdot \sin (σ T))

Go Weight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle

W body = P dynamic \cdot A \cdot C L

Go Weight of Aircraft for given Lift-to-Drag Ratio

W body = T \cdot LD

Go Weight of aircraft for given required power

W body = P \cdot \frac{C L}{V ∞ \cdot C D}

Other formulas in Thrust and Power Requirements category

Go Thrust for Level and Unaccelerated Flight

T = \frac{F D}{\cos (σ T)}

Go Thrust Angle for Unaccelerated Level Flight for given Drag

σ T = a \cos (\frac{F D}{T})

Go Thrust Angle for Unaccelerated Level Flight for given Lift

σ T = a \sin (\frac{W body - F L}{T})

Go Thrust of Aircraft required for Level, Unaccelerated Flight

T = P dynamic \cdot A \cdot C D

How to Evaluate Weight of Aircraft for given Coefficients of Lift and Drag?

Weight of Aircraft for given Coefficients of Lift and Drag evaluator uses Weight of Body = Lift Coefficient*Thrust/Drag Coefficient to evaluate the Weight of Body, The Weight of Aircraft for given Coefficients of Lift and Drag is the force exerted by gravity on the mass of the aircraft, it's a crucial parameter in aviation because it affects the aircraft's performance, including its ability to generate lift, maintain altitude, and maneuver, coefficients of lift and drag are dimensionless parameters used in aerodynamics to quantify the lift and drag forces generated by an aircraft's wings or airfoils relative to its size, shape, and flight conditions. Weight of Body is denoted by W_body symbol.

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

FAQs on Weight of Aircraft for given Coefficients of Lift and Drag

What is the formula to find Weight of Aircraft for given Coefficients of Lift and Drag?

The formula of Weight of Aircraft for given Coefficients of Lift and Drag is expressed as Weight of Body = Lift Coefficient*Thrust/Drag Coefficient. Here is an example- 3.666667 = 1.1*100/0.5.

How to calculate Weight of Aircraft for given Coefficients of Lift and Drag?

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

What are the other ways to Calculate Weight of Body?

Here are the different ways to Calculate Weight of Body-

Weight of Body=Lift Force+(Thrust*sin(Thrust Angle))
Weight of Body=Dynamic Pressure*Area*Lift Coefficient
Weight of Body=Thrust*Lift-to-Drag Ratio

Can the Weight of Aircraft for given Coefficients of Lift and Drag be negative?

No, the Weight of Aircraft for given Coefficients of Lift and Drag, measured in Force cannot be negative.

Which unit is used to measure Weight of Aircraft for given Coefficients of Lift and Drag?

Weight of Aircraft for given Coefficients of Lift and Drag is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Weight of Aircraft for given Coefficients of Lift and Drag can be measured.

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Weight of Aircraft for given Coefficients of Lift and Drag Formula

​GoWeight of Aircraft in Level, Unaccelerated Flight Formula

​GoWeight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle Formula

Weight of Aircraft for given Coefficients of Lift and Drag Example

Weight of Aircraft for given Coefficients of Lift and Drag Solution

Weight of Aircraft for given Coefficients of Lift and Drag Formula Elements

Other Formulas to find Weight of Body

Other formulas in Thrust and Power Requirements category

How to Evaluate Weight of Aircraft for given Coefficients of Lift and Drag?

FAQs on Weight of Aircraft for given Coefficients of Lift and Drag

Variable Name

GoWeight of Aircraft in Level, Unaccelerated Flight Formula

GoWeight of Aircraft for Level, Unaccelerated Flight at Negligible Thrust Angle Formula