Is there a way to calculate the correct rise or run when scaling a fuselage block manually? I tried Rise being equivalent to the larger Length divided by the Larger Diameter and the Small Diameter, or R=L/(D+d), but it didn't work
Is there a way to calculate the correct rise or run when scaling a fuselage block manually? I tried Rise being equivalent to the larger Length divided by the Larger Diameter and the Small Diameter, or R=L/(D+d), but it didn't work
so if I get this right, it's r=.125(.25(S1-S2)), where S1 is the h/w of the front and S2 is the h/w of the back?
@AgentFox123
r = 0.125 per 0.25 of difference between h/w of front end and h/w of back end.
r = rise/run
h/w = height/width
For example, a h/w of 2 at the front, a h/w of 1.75 at the back, has a rise/run of 0.125.
@ArcturusAerospace As in, The diameter of the fuselage in relation to the length to make the rise/run to make the fuselage level at the side that I want the rise run in the direction of
What do you mean?