Hi Guys,
Thanks for the trim ideas. And sorry for the late reply, I've been camped out with the Onex without a keyboard.
At this point in my Onex bonding process I need perfect flying conditions. Around here (North Central Texas) this time of year that only happens sometimes in the morning. So, I've only gotten in a couple of flights since first flight. This morning was to be the third but ... while the winds were calm there was fog and light drizzle.
Anyway, as far as the trim is concerned, I probably didn't ask the question very clearly. What I really wanted to know is where to start and how to attack the process of trimming the airplane. After some fooling around and some thought this is what I came up with.
Step One is to check the rigging. When I rigged the flaps and ailerons I simply lined them up with each other and with the wing tips. Turns out that wasn't very smart. My left wing tip is about 1.5 Deg. out of rig, re-flexed, or up. I'll just live with that for now but those who haven't attached the tips yet you would do well to check them and nudge them into rig if possible. I did re-adjust the flap to proper rig.
Step Two will be to fly the airplane straight and level with aileron and rudder. I will attempt to "fix" the heavy wing by squeezing the trailing edge of the light wing's aileron while still applying rudder as necessary to fly straight and level. I'll repeat this process until only rudder is needed to fly straight and level.
Step Three will be adding rudder trim as necessary until I can fly straight and level and drop the stick and put my feet flat on the floor and it stays put.
I really don't have a good feel as to whether or not the trim will be speed sensitive/dependent. I guess I should pick the anticipated cruse speed and perform all tests at that speed and just hope the trim is OK at other speeds.
Another problem showed up. I didn't think about it while building the fuse, but I placed my fresh air vent directly behind the left valve cover. While taxiing with the canopy cracked open the air coming in between the windshield and the canopy is noticeably cooler than the air coming through the fresh air vent. I thought it strange that the valve cover could warm the air to the point that I could feel the difference. The air continued to feel too warm throughout the flight. Then another observation: I had a small oil leak at the left valve cover gasket (the one that I didn't replace a couple of weeks ago). The flange of the valve cover is inside the plane of the cowl side yet the oil didn't show up inside the cowl. It showed up as streaks down the side of the airplane. The streaks are centered about the fresh air vent. Although the valve covers are on the low pressure side of the baffling it appears that cylinder cooling air is being sucked out around the cutouts in the cowl sides. Not good. I should point out that my cowl exit isn't per plans. That's a side effect of my Hummel installation. I have no idea if the same situation exists with the standard cowl exit.
A pic of the cutout showing the valve cover flanges inside the cowl:
A pic showing the oil streaks down the fuse side:
After I get the airplane trimmed out I'll work on the geometry of the cowl exit and see if I can get enough suck to keep the cylinder head cooling air out of the cockpit. In the mean time I have installed a CO sensor and a "Slip/Skid" to the instrument panel to support further testing. I have a manometer on order to test various cowl exit geometries.
More fancy instruments :-):
Forever Forward,
Wes