Sideslip angle Solution

STEP 0: Pre-Calculation Summary
Formula Used
Sideslip Angle = asin(Velocity Along Pitch Axis/(sqrt((Velocity Along Roll Axis^2)+(Velocity Along Pitch Axis^2)+(Velocity Along Yaw Axis^2))))
β = asin(v/(sqrt((u^2)+(v^2)+(w^2))))
This formula uses 3 Functions, 4 Variables
Functions Used
sin - Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse., sin(Angle)
asin - The inverse sine function, is a trigonometric function that takes a ratio of two sides of a right triangle and outputs the angle opposite the side with the given ratio., asin(Number)
sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)
Variables Used
Sideslip Angle - (Measured in Radian) - The Sideslip Angle, also called the angle of sideslip, is a term used in fluid dynamics and aerodynamics, and aviation which relates to the rotation of the aircraft centerline from the relative wind.
Velocity Along Pitch Axis - (Measured in Meter per Second) - Velocity Along Pitch Axis is the component of velocity along the pitch axis of the aircraft.
Velocity Along Roll Axis - (Measured in Meter per Second) - Velocity Along Roll Axis is the component of velocity along the roll axis of the aircraft.
Velocity Along Yaw Axis - (Measured in Meter per Second) - Velocity Along Yaw Axis is the component of velocity along the yaw axis of the aircraft.
STEP 1: Convert Input(s) to Base Unit
Velocity Along Pitch Axis: 0.88 Meter per Second --> 0.88 Meter per Second No Conversion Required
Velocity Along Roll Axis: 17 Meter per Second --> 17 Meter per Second No Conversion Required
Velocity Along Yaw Axis: 0.4 Meter per Second --> 0.4 Meter per Second No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
β = asin(v/(sqrt((u^2)+(v^2)+(w^2)))) --> asin(0.88/(sqrt((17^2)+(0.88^2)+(0.4^2))))
Evaluating ... ...
β = 0.0517042589880967
STEP 3: Convert Result to Output's Unit
0.0517042589880967 Radian -->2.96243582286985 Degree (Check conversion ​here)
FINAL ANSWER
2.96243582286985 2.962436 Degree <-- Sideslip Angle
(Calculation completed in 00.020 seconds)

Credits

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Created by Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
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Verified by Shikha Maurya
Indian Institute of Technology (IIT), Bombay
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Sideslip angle Formula

​LaTeX ​Go
Sideslip Angle = asin(Velocity Along Pitch Axis/(sqrt((Velocity Along Roll Axis^2)+(Velocity Along Pitch Axis^2)+(Velocity Along Yaw Axis^2))))
β = asin(v/(sqrt((u^2)+(v^2)+(w^2))))

What angle does a plane fly at?

An aircraft typically flies at angles of attack range of about 2-5 degrees, depending on the flight altitude, speed and g-load of manoeuvre. It's much more (about 10-12 degrees) when flight speed is near to take-off and landing speed.

How to Calculate Sideslip angle?

Sideslip angle calculator uses Sideslip Angle = asin(Velocity Along Pitch Axis/(sqrt((Velocity Along Roll Axis^2)+(Velocity Along Pitch Axis^2)+(Velocity Along Yaw Axis^2)))) to calculate the Sideslip Angle, Sideslip angle is a measure of an object's rotation or deviation from its intended direction of motion, commonly used in aerodynamics and aerospace engineering to describe the angle between an aircraft's velocity vector and its direction of motion. Sideslip Angle is denoted by β symbol.

How to calculate Sideslip angle using this online calculator? To use this online calculator for Sideslip angle, enter Velocity Along Pitch Axis (v), Velocity Along Roll Axis (u) & Velocity Along Yaw Axis (w) and hit the calculate button. Here is how the Sideslip angle calculation can be explained with given input values -> 169.7351 = asin(0.88/(sqrt((17^2)+(0.88^2)+(0.4^2)))).

FAQ

What is Sideslip angle?
Sideslip angle is a measure of an object's rotation or deviation from its intended direction of motion, commonly used in aerodynamics and aerospace engineering to describe the angle between an aircraft's velocity vector and its direction of motion and is represented as β = asin(v/(sqrt((u^2)+(v^2)+(w^2)))) or Sideslip Angle = asin(Velocity Along Pitch Axis/(sqrt((Velocity Along Roll Axis^2)+(Velocity Along Pitch Axis^2)+(Velocity Along Yaw Axis^2)))). Velocity Along Pitch Axis is the component of velocity along the pitch axis of the aircraft, Velocity Along Roll Axis is the component of velocity along the roll axis of the aircraft & Velocity Along Yaw Axis is the component of velocity along the yaw axis of the aircraft.
How to calculate Sideslip angle?
Sideslip angle is a measure of an object's rotation or deviation from its intended direction of motion, commonly used in aerodynamics and aerospace engineering to describe the angle between an aircraft's velocity vector and its direction of motion is calculated using Sideslip Angle = asin(Velocity Along Pitch Axis/(sqrt((Velocity Along Roll Axis^2)+(Velocity Along Pitch Axis^2)+(Velocity Along Yaw Axis^2)))). To calculate Sideslip angle, you need Velocity Along Pitch Axis (v), Velocity Along Roll Axis (u) & Velocity Along Yaw Axis (w). With our tool, you need to enter the respective value for Velocity Along Pitch Axis, Velocity Along Roll Axis & Velocity Along Yaw Axis and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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