How to Calculate Tail lift for given tail pitching moment?
Tail lift for given tail pitching moment calculator uses Lift due to tail = -Pitching Moment due to Tail/Horizontal tail moment arm to calculate the Lift due to tail, The Tail lift for given tail pitching moment is a function of the pitching moment due to the tail and the moment arm (distance between tail lift center and center of gravity of aircraft). Lift due to tail is denoted by Lt symbol.
How to calculate Tail lift for given tail pitching moment using this online calculator? To use this online calculator for Tail lift for given tail pitching moment, enter Pitching Moment due to Tail (Mt) & Horizontal tail moment arm (𝒍t) and hit the calculate button. Here is how the Tail lift for given tail pitching moment calculation can be explained with given input values -> 273.0375 = -(-218.43)/0.8.