>I know we have discussed this before. I'm loosing almost
>all line tension above 45 degrees especially in the
>overheads and V8. Level line tension is good. Here's my set
>up on the Harbinger:
>625 sq
>52 oz
>SSW ASP 53
>BE 2 blade W 12 1/5 x 4.2 launched at 8900
>lap time 5.2 to 5.3
>wings level upright and inverted
>1 3/4 to 2 oz tip weight
>airplane checked for trueness and stab tilt
>63 foot eye to eye .018 lines
>3/4 longer inboard wing V outboard wing
>outboard flap area is about 2% larger in area V inboard flap
>moving the LO all over the place doesn't seem to help a lot
>cg at about 24 to 25%
OK. Sounds pretty good.
1. Accurately measure your CG point. ACCURATELY. Use a CG Machine or something similar. Measure this point from the hingeline. Measure forward at the tip from the hingeline and mark this point with a ren written on a piece of clear tape. Cover this tape with a another piece (it is fuelproof now and can be removed later).
2. Move the leadouts to 1.25" behind this point.
3. Add another 3/4 oz of tip weight. Making the total 2.5 oz (Paul Walker would kill me). You may not realize how much tip weight will be required if the outboard flap is LARGER than the inboard. Especially with these new high thrust engines. I think the larger outboard flap is mostly required when airplanes slows in the corner a lot. Most of the new engines slow much less. The four cycle almost does not slow down at all.
4. Look for hinging in the hard bottom corners (obviously that is a lot of tip weight). Hit some hard corner bottoms.
Look for line tension up top. You should see a noticable increase.
Look for "lurching" (Al Rabe word--love it). That is when the airplane does not turn where you tell it too. It turns late and "slides" before it turns.
Both hinging and lurching are symptoms of too much tip weight. If neither are present ADD MORE TIP WEIGHT.
Hinging is the most severe symptom of excessive tip weight. Hinging will require 1/4 oz removed or more.
If lurching is present but not hinging, remove little "chips" of lead at a time, it won't take much to hit the spot where the lurching stops.
Once this is done and the airplane is somewhat satisfactory (the overhead tension should be adequate). Move the leadouts forward 1/8" of an inch at a time. The overhead tension should maximize at some point between 1.25" and 3/4" behind the CG.
Also the corner entry will "clean up" some.
Do not be tempted to move the leadouts too far forward to get a lot of overhead tension. Foward leadouts can cause a lot of weird "funnies" especially in the wind.
>I used a fixed adjustable rudder with little help then
>hooked up a Rabe rudder. It gives no left rudder on the
>insides but gives good right rudder on the outsides. When I
>do the O8, the inside line tension is very soft, but the
>outside line tension is good.
>
>Any ideas that I could try?
Set the rudder fixed and nuetral for all of the above. You can hook it back up when you are through with the above process and use it to optimize again.