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 formula is defined as a measure of how an upward gust of wind affects the angle of attack of an aircraft, influencing its lift and overall aerodynamic performance during flight maneuvers. 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.