- #1

- 75

- 0

[itex]\frac{\dot{\phi^2}}{2g}R^2[/itex]

where

[itex]R[/itex] - radius from center of fuselage

[itex]g[/itex] - gravitational constant

[itex]\dot{\phi}[/itex] - roll rate

my question is where does the "2" next to the gravitational constant come from?