Change in Angle of Attack due to Upward Gust evaluator uses Change in Angle of Attack = tan(Gust Velocity/Flight Velocity) to evaluate the Change in Angle of Attack, Change in Angle of Attack due to Upward Gust refers to the alteration in the angle of attack experienced by an aircraft when encountering a sudden upward gust of wind. This change is calculated using the provided formula, which relates the gust velocity to the flight velocity. Understanding and accounting for this change is crucial for ensuring the stability and control of the aircraft, especially during turbulent conditions. Change in Angle of Attack is denoted by Δα symbol.
How to evaluate Change in Angle of Attack due to Upward Gust using this online evaluator? To use this online evaluator for Change in Angle of Attack due to Upward Gust, enter Gust Velocity (u) & Flight Velocity (V) and hit the calculate button.