Larry Foster · Jun 12, 2003 02:27 PM
#0 sourceCurrently the best overall performance is with the forward lead out 1/8" behind the CG, 1/2 oz of wing tip weight and the CG is 6.2 inches forward of the trailing edge (hinge line).
Here's what I've tried so far:
Reducing wing tip weight until total loss of line tension at 45 deg. 1/4 oz at a time, also adding until a hinge was noticed in a hard pullout.
Moved lead outs from front to back 1/8" at a time, from 1/2 in front of CG to 3/4" rear of CG.
Added tail weight until plane was unstable in level flight.
Added nose weight until it was extremely difficult to turn.
Tweaking the out board flap up until the outboard wing was flying down in level flight.
I changed tip weight 4 times with each lead out change. Total of 16 flights
Nose weight helped over all line tension but not the problem.
Tail weight reduced line tension but did not help the problem.
The Rudder is air foiled per plans
The airframe was put together with a jig and all points are square, I checked them again today.
Here is the true effective wing and flap area as measured from the plane. Flaps are averaged over 8 points and wing is averaged over 12 points.
The inboard wing is 2" longer than the outboard
Inboard sq in-------- Outboard sq in
Wing-213.5--------------195.9
Flap--41.8---------------43.2
Total effective wing area is: 494.4 sq in
Using three points to measure the wing it comes to 535 sq in. (Root and tip / 2 X length)
Model weighs 37.0 oz (weighed at the Post Office)
Larry
Sammy