Weight of aircraft during ground roll evaluator uses Weight = (Rolling Resistance/Coefficient of Rolling Friction)+Lift to evaluate the Weight, Weight of Aircraft During Ground Roll is a measure of the total weight of an aircraft during the ground roll phase of takeoff, calculated by considering the rolling resistance, friction coefficient, and lift force, providing a crucial parameter for aircraft performance and safety analysis. Weight is denoted by W symbol.
How to evaluate Weight of aircraft during ground roll using this online evaluator? To use this online evaluator for Weight of aircraft during ground roll, enter Rolling Resistance (R), Coefficient of Rolling Friction (μr) & Lift (FL) and hit the calculate button.