How to Calculate Aerodynamic Normal Force?
Aerodynamic Normal Force calculator uses Aerodynamic Normal Force = Normal Force Coefficient*Dynamic Pressure*Reference Area to calculate the Aerodynamic Normal Force, Aerodynamic Normal Force is a measure of the force exerted by the air pressure on an object, perpendicular to the surface of the object, resulting from the air's resistance to the object's motion, it is a crucial concept in aerodynamics, essential for understanding and predicting the behavior of aircraft, wind turbines, and other systems interacting with air. Aerodynamic Normal Force is denoted by Z symbol.
How to calculate Aerodynamic Normal Force using this online calculator? To use this online calculator for Aerodynamic Normal Force, enter Normal Force Coefficient (Cz), Dynamic Pressure (q) & Reference Area (S) and hit the calculate button. Here is how the Aerodynamic Normal Force calculation can be explained with given input values -> 19.304 = 0.38*10*5.08.