Glide angle for given lift-to-drag ratio Calculator

✖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.ⓘ Lift-to-drag Ratio [LD]

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✖Glide Angle is defined as the angle made by the glide flight path with the horizontal.ⓘ Glide angle for given lift-to-drag ratio [θ]

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Glide angle for given lift-to-drag ratio Solution

STEP 0: Pre-Calculation Summary

Formula Used

Glide Angle = atan(1/Lift-to-drag Ratio)
θ = atan(1/LD)
This formula uses 2 Functions, 2 Variables

Functions Used

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., 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., atan(Number)

Variables Used

Glide Angle - (Measured in Radian) - Glide Angle is defined as the angle made by the glide flight path with the horizontal.
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.

STEP 1: Convert Input(s) to Base Unit

Lift-to-drag Ratio: 6.61 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

θ = atan(1/LD) --> atan(1/6.61)

Evaluating ... ...

θ = 0.150147343396535

STEP 3: Convert Result to Output's Unit

0.150147343396535 Radian --> No Conversion Required

FINAL ANSWER

0.150147343396535 ≈ 0.150147 Radian <-- Glide Angle

(Calculation completed in 00.004 seconds)

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Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

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< Gliding Flight Calculators

Glide angle

LaTeX Go Glide Angle = atan(Drag Force/Lift Force)

Lift Force for given Glide Angle

LaTeX Go Lift Force = Drag Force/tan(Glide Angle)

Drag for given Glide Angle

LaTeX Go Drag Force = Lift Force*tan(Glide Angle)

Lift-to-drag ratio for given glide angle

LaTeX Go Lift-to-drag Ratio = 1/tan(Glide Angle)

Glide angle for given lift-to-drag ratio Formula

LaTeX Go

Glide Angle = atan(1/Lift-to-drag Ratio)
θ = atan(1/LD)

How is the glide ratio affected?

The glide ratio is affected by all of the four fundamental forces that act on an aircraft in flight - lift, drag, weight, and thrust.

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

Glide angle for given lift-to-drag ratio calculator uses Glide Angle = atan(1/Lift-to-drag Ratio) to calculate 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 calculate Glide angle for given lift-to-drag ratio using this online calculator? To use this online calculator for Glide angle for given lift-to-drag ratio, enter Lift-to-drag Ratio (LD) and hit the calculate button. Here is how the Glide angle for given lift-to-drag ratio calculation can be explained with given input values -> 0.02702 = atan(1/6.61).

FAQ

What is Glide angle for given lift-to-drag ratio?

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 and is represented as θ = atan(1/LD) or Glide Angle = atan(1/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.

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

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 is calculated using Glide Angle = atan(1/Lift-to-drag Ratio). To calculate Glide angle for given lift-to-drag ratio, you need Lift-to-drag Ratio (LD). With our tool, you need to enter the respective value for Lift-to-drag Ratio and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Glide Angle?

In this formula, Glide Angle uses Lift-to-drag Ratio. We can use 1 other way(s) to calculate the same, which is/are as follows -

Glide Angle = atan(Drag Force/Lift Force)

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