Lift Force for given Glide Angle 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
FL=FDtan(θ)
FL - Lift Force?FD - Drag Force?θ - Glide Angle?

Lift Force for given Glide Angle Example

With values
With units
Only example

Here is how the Lift Force for given Glide Angle equation looks like with Values.

Here is how the Lift Force for given Glide Angle equation looks like with Units.

Here is how the Lift Force for given Glide Angle equation looks like.

99.9767Edit=15.11Edittan(0.15Edit)
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Lift Force for given Glide Angle Solution

Follow our step by step solution on how to calculate Lift Force for given Glide Angle?

FIRST Step Consider the formula
FL=FDtan(θ)
Next Step Substitute values of Variables
FL=15.11Ntan(0.15rad)
Next Step Prepare to Evaluate
FL=15.11tan(0.15)
Next Step Evaluate
FL=99.9766976494641N
LAST Step Rounding Answer
FL=99.9767N

Lift Force for given Glide Angle Formula Elements

Variables
Functions
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: FL
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Drag Force
Drag Force is the resisting force experienced by an object moving through a fluid.
Symbol: FD
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Glide Angle
Glide Angle is defined as the angle made by the glide flight path with the horizontal.
Symbol: θ
Measurement: AngleUnit: rad
Note: Value can be positive or negative.
tan
The tangent of an angle is a trigonometric ratio of the length of the side opposite an angle to the length of the side adjacent to an angle in a right triangle.
Syntax: tan(Angle)

Other formulas in Gliding Flight category

​Go Lift-to-drag ratio for given glide angle
LD=1tan(θ)
​Go Drag for given Glide Angle
FD=FLtan(θ)
​Go Glide angle
θ=atan(FDFL)
​Go Glide angle for given lift-to-drag ratio
θ=atan(1LD)

How to Evaluate Lift Force for given Glide Angle?

Lift Force for given Glide Angle evaluator uses Lift Force = Drag Force/tan(Glide Angle) to evaluate the Lift Force, The Lift force for given glide angle equation is derived from the relationship between lift force, drag force, and glide angle in gliding flight. It shows that the lift force is proportional to the drag force and inversely proportional to the tangent of the glide angle, using this equation, you can determine the lift force required to sustain a particular glide angle during gliding flight. Lift Force is denoted by FL symbol.

How to evaluate Lift Force for given Glide Angle using this online evaluator? To use this online evaluator for Lift Force for given Glide Angle, enter Drag Force (FD) & Glide Angle (θ) and hit the calculate button.

FAQs on Lift Force for given Glide Angle

What is the formula to find Lift Force for given Glide Angle?
The formula of Lift Force for given Glide Angle is expressed as Lift Force = Drag Force/tan(Glide Angle). Here is an example- 43.73567 = 15.11/tan(0.15).
How to calculate Lift Force for given Glide Angle?
With Drag Force (FD) & Glide Angle (θ) we can find Lift Force for given Glide Angle using the formula - Lift Force = Drag Force/tan(Glide Angle). This formula also uses Tangent (tan) function(s).
Can the Lift Force for given Glide Angle be negative?
No, the Lift Force for given Glide Angle, measured in Force cannot be negative.
Which unit is used to measure Lift Force for given Glide Angle?
Lift Force for given Glide Angle is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Lift Force for given Glide Angle can be measured.
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