How to Calculate Tail Pitching moment coefficient?
Tail Pitching moment coefficient calculator uses Tail Pitching Moment Coefficient = Pitching Moment due to Tail/(0.5*Freestream Density*Flight Velocity^2*Reference Area*Mean aerodynamic chord) to calculate the Tail Pitching Moment Coefficient, The Tail Pitching moment coefficient for a horizontal tail is a function of the pitching moment of the tail, the altitude of the aircraft, the wing's velocity, and the mean aerodynamic chord of the wing. Tail Pitching Moment Coefficient is denoted by Cmt symbol.
How to calculate Tail Pitching moment coefficient using this online calculator? To use this online calculator for Tail Pitching moment coefficient, enter Pitching Moment due to Tail (Mt), Freestream Density (ρ∞), Flight Velocity (V), Reference Area (S) & Mean aerodynamic chord (cma) and hit the calculate button. Here is how the Tail Pitching moment coefficient calculation can be explained with given input values -> -0.600014 = (-218.43)/(0.5*1.225*30^2*5.08*0.2).