BVM Bobcat Composite Flap settings
#2

Jay
Didn't use the gauge, but mine is set :- Balance back 15mm from the boom dots
Take off flap TE root section 25mm (1") and 3mm (1/8") up mixed in.
Landing flap TE root section 90mm (3 5/8") and 7mm (bit more than 1/4") up mixed in.
Any CROW and you can reduce the elevator up compensation
Dave
Didn't use the gauge, but mine is set :- Balance back 15mm from the boom dots
Take off flap TE root section 25mm (1") and 3mm (1/8") up mixed in.
Landing flap TE root section 90mm (3 5/8") and 7mm (bit more than 1/4") up mixed in.
Any CROW and you can reduce the elevator up compensation
Dave
Last edited by Dave Wilshere; 11-19-2015 at 04:58 AM.
#7

Yep! basically, it dumps lift. Effect can be different depending on the wing section and aileron cord ratio. It changes the wing incidence on that portion of wing, so it works well on something like a Classic Flash as it changes the angle the airframe flies at, raising the nose, so adding drag, the nice fat wing section still has plenty of lift.
For me the Bobcat has plenty of drag from the flaps, so like the UF I don't like CROW on these.
For me the Bobcat has plenty of drag from the flaps, so like the UF I don't like CROW on these.
Last edited by Dave Wilshere; 11-19-2015 at 11:48 AM.
#9
Thread Starter

My Feedback: (57)
How much crow did you use c/f? Currently I did 15 degree flap for T/O, 35 for landing with 3/8" aileron up (crow) on each side. Mr Matt, you are correct on all, & in addition it acts as a form of mechanical washout (as Dave said), so in theory it will help almost any aircraft maintain aileron (roll axis) control at a slightly higher angle of attack (reducing stall speed) than without.. & it's fun to program & cool..lol




