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Total Lift of Wing-Tail Combination Formula

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The Lift Force, lifting force or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow. Check FAQs

F L = L w + L t

F_L - Lift Force?L_w - Lift due to Wing?L_t - Lift due to Tail?

Total Lift of Wing-Tail Combination Example

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Here is how the Total Lift of Wing-Tail Combination equation looks like with Values.

Here is how the Total Lift of Wing-Tail Combination equation looks like with Units.

Here is how the Total Lift of Wing-Tail Combination equation looks like.

1073.04 = 800 + 273.04

1073.04N = 800N + 273.04N

1073.04 = 800 + 273.04

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Total Lift of Wing-Tail Combination Solution

Follow our step by step solution on how to calculate Total Lift of Wing-Tail Combination?

FIRST Step Consider the formula

F L = L w + L t

Next Step Substitute values of Variables

∴

F L = 800N + 273.04N

Next Step Prepare to Evaluate

∴

F L = 800 + 273.04

LAST Step Evaluate

∴

F L = 1073.04N

Total Lift of Wing-Tail Combination Formula Elements

Variables

Lift Force

The Lift Force, lifting force or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow.

Symbol: F_L

Measurement: ForceUnit: N

Note: Value should be greater than 0.

Formulas to find Lift Force

Lift due to Wing

Lift due to Wing is the lift force acting on the wing (only) of an aircraft.

Symbol: L_w

Measurement: ForceUnit: N

Note: Value can be positive or negative.

Formulas to find Lift due to Wing

Lift due to Tail

Lift due to Tail refers to the aerodynamic force generated by the horizontal stabilizer of an aircraft.

Symbol: L_t

Measurement: ForceUnit: N

Note: Value can be positive or negative.

Formulas to find Lift due to Tail

Other formulas in Wing Tail Contribution category

Go Angle of Attack at Tail

α t = α w - 𝒊 w - ε + 𝒊 t

Go Angle of Attack of Wing

α w = α t + 𝒊 w + ε - 𝒊 t

Go Angle of incidence of wing

𝒊 w = α w - α t - ε + 𝒊 t

Go Downwash angle

ε = α w - 𝒊 w - α t + 𝒊 t

How to Evaluate Total Lift of Wing-Tail Combination?

Total Lift of Wing-Tail Combination evaluator uses Lift Force = Lift due to Wing+Lift due to Tail to evaluate the Lift Force, Total Lift of Wing-Tail Combination is a measurement of the combined upward force exerted by the wing and tail of an aircraft, influencing its stability and performance during flight, calculated by summing the individual lift forces generated by the wing and tail components. Lift Force is denoted by F_L symbol.

How to evaluate Total Lift of Wing-Tail Combination using this online evaluator? To use this online evaluator for Total Lift of Wing-Tail Combination, enter Lift due to Wing (L_w) & Lift due to Tail (L_t) and hit the calculate button.

FAQs on Total Lift of Wing-Tail Combination

What is the formula to find Total Lift of Wing-Tail Combination?

The formula of Total Lift of Wing-Tail Combination is expressed as Lift Force = Lift due to Wing+Lift due to Tail. Here is an example- 1073.04 = 800+273.04.

How to calculate Total Lift of Wing-Tail Combination?

With Lift due to Wing (L_w) & Lift due to Tail (L_t) we can find Total Lift of Wing-Tail Combination using the formula - Lift Force = Lift due to Wing+Lift due to Tail.

Can the Total Lift of Wing-Tail Combination be negative?

No, the Total Lift of Wing-Tail Combination, measured in Force cannot be negative.

Which unit is used to measure Total Lift of Wing-Tail Combination?

Total Lift of Wing-Tail Combination is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Total Lift of Wing-Tail Combination can be measured.

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Total Lift of Wing-Tail Combination Formula

Total Lift of Wing-Tail Combination Example

Total Lift of Wing-Tail Combination Solution

Total Lift of Wing-Tail Combination Formula Elements

Other formulas in Wing Tail Contribution category

How to Evaluate Total Lift of Wing-Tail Combination?

FAQs on Total Lift of Wing-Tail Combination

Variable Name