Fin Volume Ratio/Coefficient Calculator

Fin Volume Ratio/Coefficient Calculator

Where:-

SF is the vertical fin (Vertical Tail) area

lf is the Tail lift arm

S is the Wing Area

b is the Wing Span

Fins are the small Auxiliary Airfoil Mounted at the top and bottom of the Fuselage at the Rear end.

NOTE:- Vertical Fin Contributes Positively for Directional Stability

Chandan Singh