B Model Elevator Trim Tab
Posted: Fri Apr 15, 2022 10:53 pm
I've read some previous posts about elevator trim tabs, but....
I have installed a conventional trim tab to the inboard portion of the left elevator of my B Model Sonex. It is just less than half the elevator width by about 2.5 inches. With flaps retracted it works fine (although it is not very sensitive), but it will not hold the nose up with full flap. So I built a new tab which is twice as big (i.e. same hinge point but it protrudes nearly 3 inches behind the original trailing edge of the elevator). I also increased the length of the tab lever arm, so there is more trim tab angle available.
Qualitatively, with full nose up trim, the full flap stick forces are about the same. That is, doubling the trim tab area and increasing its angle has had no noticeable effect.
Does anyone have similar experience or a reason why there is no improvement?
Given little or no change in stick force, the moment generated by both tabs must be about the same, (and not very much). Does it suggest that there is little (or separated) airflow over the inboard trailing edge of the elevator (at least with full flap)?
Has anyone made a full width trim tab for the elevator? If so, did it work and what was the size?
Has anyone tried vortex generators on the horizontal stabilizer or the elevator?
DK
I have installed a conventional trim tab to the inboard portion of the left elevator of my B Model Sonex. It is just less than half the elevator width by about 2.5 inches. With flaps retracted it works fine (although it is not very sensitive), but it will not hold the nose up with full flap. So I built a new tab which is twice as big (i.e. same hinge point but it protrudes nearly 3 inches behind the original trailing edge of the elevator). I also increased the length of the tab lever arm, so there is more trim tab angle available.
Qualitatively, with full nose up trim, the full flap stick forces are about the same. That is, doubling the trim tab area and increasing its angle has had no noticeable effect.
Does anyone have similar experience or a reason why there is no improvement?
Given little or no change in stick force, the moment generated by both tabs must be about the same, (and not very much). Does it suggest that there is little (or separated) airflow over the inboard trailing edge of the elevator (at least with full flap)?
Has anyone made a full width trim tab for the elevator? If so, did it work and what was the size?
Has anyone tried vortex generators on the horizontal stabilizer or the elevator?
DK