How to Calculate Mean Aerodynamic Chord for Propeller-Driven Airplane?
Mean Aerodynamic Chord for Propeller-Driven Airplane calculator uses Mean Aerodynamic Chord = (1/Reference Area)*int(Chord Length^2,x,-Wingspan/2,Wingspan/2) to calculate the Mean Aerodynamic Chord, Mean Aerodynamic Chord for Propeller-Driven Airplane is a mathematical representation that determines the average aerodynamic chord of a propeller-driven airplane, which is a crucial parameter in assessing its aerodynamic performance, by integrating the squared chord length over the entire wing span. Mean Aerodynamic Chord is denoted by cma symbol.
How to calculate Mean Aerodynamic Chord for Propeller-Driven Airplane using this online calculator? To use this online calculator for Mean Aerodynamic Chord for Propeller-Driven Airplane, enter Reference Area (S), Chord Length (Lc) & Wingspan (b) and hit the calculate button. Here is how the Mean Aerodynamic Chord for Propeller-Driven Airplane calculation can be explained with given input values -> 142.126 = (1/5.08)*int(3.8^2,x,-50/2,50/2).