Elsewhere I’ve been accused of going overboard. ? Maybe so, but in my threads I not only try to show what I do but explain why I did what I did. If the thread is a build thread I then try to show what worked or didn’t. I also try to show any issues I may have overlooked.
To the “V” tail angle I changed it to 99° as I wanted a ship that could track well through a loop or a pylon turn. Historically “V” tail have lacked directional control. When I see 110° I think the designer may not have given this angle much thought. I know the "V”-tail angle is highly dependent on the aspect ratio of the wing. I also know that there is an inverse relationship for the need of vertical fin area and dihedral when looking for directional stability.
As I knew I wanted to lower the dihedral to get a more neutral feel on the slope with the typical cross winds. I knew I’d want more fin area as a result of lowering the dihedral. This and the fact that I think 110° is too flat for the long wings and short fuselage, I increased the fin area by bringing the inclusive “V” tail angle down to 99°. Was this needed? NO, there are plenty of Mefistos flying just fine, even great at 110°.
I will say that my Mefisto has the strongest “V”-tail rudder response of any “V”-tail I own. Well, she is second only to the DJ Aerotech Chrysalis F3-RES. But the F3-RES class is a rudder elevator class, and one would want a very strong rudder response with that class of glider.
As to decalage, I would add a 0.7mm shim to the front of the LE of the “V”-tail mount with the S6063 airfoil. (Note; that the “V”-tail actually pivots mid span on the fuselage mount). This is because the S6063 airfoil at speed does not need much incidence. Because the tail boom will whip on hard landings this will place a lot of load on the “V” tail glue joint. I would add this shim during the build because one should glass the “V” tail with many layers to make a solid mount. With a glassed on “V”tail one really doesn’t get a good opportunity to try to re-shim the “V”-tail as part on one’s flight testing.
If one wants to experiment with the decalage a bolt on tail might be a nice option.
Your friendly engineering type,
Konrad