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Glide Angle is defined as the angle made by the glide flight path with the horizontal. Check FAQs
θ=atan(1LD)
θ - Glide Angle?LD - Lift-to-drag Ratio?

Glide angle for given lift-to-drag ratio Example

With values
With units
Only example

Here is how the Glide angle for given lift-to-drag ratio equation looks like with Values.

Here is how the Glide angle for given lift-to-drag ratio equation looks like with Units.

Here is how the Glide angle for given lift-to-drag ratio equation looks like.

0.1501Edit=atan(16.61Edit)
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Glide angle for given lift-to-drag ratio Solution

Follow our step by step solution on how to calculate Glide angle for given lift-to-drag ratio?

FIRST Step Consider the formula
θ=atan(1LD)
Next Step Substitute values of Variables
θ=atan(16.61)
Next Step Prepare to Evaluate
θ=atan(16.61)
Next Step Evaluate
θ=0.150147343396535rad
LAST Step Rounding Answer
θ=0.1501rad

Glide angle for given lift-to-drag ratio Formula Elements

Variables
Functions
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.
Lift-to-drag Ratio
The Lift-to-drag ratio is the amount of lift generated by a wing or vehicle, divided by the aerodynamic drag it creates by moving through the air.
Symbol: LD
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
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)
atan
Inverse tan is used to calculate the angle by applying the tangent ratio of the angle, which is the opposite side divided by the adjacent side of the right triangle.
Syntax: atan(Number)

Other Formulas to find Glide Angle

​Go Glide angle
θ=atan(FDFL)

Other formulas in Gliding Flight category

​Go Lift Force for given Glide Angle
FL=FDtan(θ)
​Go Lift-to-drag ratio for given glide angle
LD=1tan(θ)
​Go Drag for given Glide Angle
FD=FLtan(θ)
​Go Weight of Glider
Wg=FLcos(θ)+FDsin(θ)

How to Evaluate Glide angle for given lift-to-drag ratio?

Glide angle for given lift-to-drag ratio evaluator uses Glide Angle = atan(1/Lift-to-drag Ratio) to evaluate the Glide Angle, The Glide angle for given lift-to-drag ratio equation provides the glide angle corresponding to the given lift-to-drag ratio. It's an essential parameter for pilots to optimize the aircraft's glide performance and plan safe landing approaches, especially during gliding or emergency situations, the inverse tangent function allows you to find the angle whose tangent is equal to the inverse of the lift-to-drag ratio. Glide Angle is denoted by θ symbol.

How to evaluate Glide angle for given lift-to-drag ratio using this online evaluator? To use this online evaluator for Glide angle for given lift-to-drag ratio, enter Lift-to-drag Ratio (LD) and hit the calculate button.

FAQs on Glide angle for given lift-to-drag ratio

What is the formula to find Glide angle for given lift-to-drag ratio?
The formula of Glide angle for given lift-to-drag ratio is expressed as Glide Angle = atan(1/Lift-to-drag Ratio). Here is an example- 0.02702 = atan(1/6.61).
How to calculate Glide angle for given lift-to-drag ratio?
With Lift-to-drag Ratio (LD) we can find Glide angle for given lift-to-drag ratio using the formula - Glide Angle = atan(1/Lift-to-drag Ratio). This formula also uses Tangent (tan), Inverse Tan (atan) function(s).
What are the other ways to Calculate Glide Angle?
Here are the different ways to Calculate Glide Angle-
  • Glide Angle=atan(Drag Force/Lift Force)OpenImg
Can the Glide angle for given lift-to-drag ratio be negative?
Yes, the Glide angle for given lift-to-drag ratio, measured in Angle can be negative.
Which unit is used to measure Glide angle for given lift-to-drag ratio?
Glide angle for given lift-to-drag ratio is usually measured using the Radian[rad] for Angle. Degree[rad], Minute[rad], Second[rad] are the few other units in which Glide angle for given lift-to-drag ratio can be measured.
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