How to Calculate Vertical tail angle of attack?
Vertical tail angle of attack calculator uses Vertical tail angle of attack = Sidewash angle+Sideslip angle to calculate the Vertical tail angle of attack, The Vertical tail angle of attack of an aircraft is the angle between the line of the chord of an aerofoil and the relative airflow. Vertical tail angle of attack is denoted by αv symbol.
How to calculate Vertical tail angle of attack using this online calculator? To use this online calculator for Vertical tail angle of attack, enter Sidewash angle (σ) & Sideslip angle (β) and hit the calculate button. Here is how the Vertical tail angle of attack calculation can be explained with given input values -> 0.117 = 0.067+0.05.