Sero
Elite member
I see you are using flaps but no landing gear, I'm guessing there isn't an issue with the flaps dragging on the ground at all being that the under wing vent helps. And are those split flaps? And it also looks like you use Master Airscrew props, What's your thoughts on those?
I am trying to figure if the advantage for the under camber tips out weighs the aerodynamic gains of a speed wing like what you are sowing me and what I have seen nn build. I did watch a couple of his vids today, the one you posted and a speed wing specific build vid, and his Mig 3 maiden. Seems the drag of the under camber is more of an disadvantage then the gains of reducing tip stall. Maybe its just that I haven't flown a speed wing yet. If i build one what should I expect?
@Headbang is not a big fan of warbirds so I have an idea of what he will say, actually he told me to build a Mig 3 lol, so it's hard to tell lol.
I see you have Canadian roundels on you Stang as well, where do you live?
Yes with the Mustang the flaps don't drag due to the bottom vent. With the Racer I'll retract to half flaps just before touch down. If your using flaps its good to have the servo arms pointing as far forward as possible so the linkage rods as near parallel to the arms when fully deployed, this will keep the strain off your servo gears if the flaps hit something. Let me know if this doesn't make sense and you need me to elaborate.
I really quite like the speed wing, everybody has covered the differences well. It definitely is not for the new flyer. On a maiden after trimming I go through a few things to learn the characteristics of the plane including what it does at stall, i highly recommend this with the speed wing.
When designing and building a plane with an airfoiled tail I try to keep tail weight in mind as much as possible. Moving the tail servos forward, substituting hot glue with a lighter option or using less glue. It all helps. Also It most cases I use bigger motors and ESCs too which obviously helps a lot.
Im near Vancouver BC.