by painless » Sat Mar 23, 2013 11:55 pm
Ed and John:
What I did is make the bottom cutouts for wing attach bolts as did Ed in a blank of 1/4" ply. Then I clamped this to the end rib of the center section with its bottom edge flush to the bottom of the center section. I simply traced the outline of the center section onto this blank, placing a piece if 1/16 ply on the top of the center section end rib to simulate the thickness of the tank.
When I join this rib to the leading and trailing edges of the wing panel, I will then bolt the spars to the center section as Ed did and raise the wing panel up to the designed 1.5 degrees. I'll space off the end rib from the center section about 1/8" at the same time. Doing all this will result in the end rib of the wing panel being parallel to that of the center section, with the wing panel dihedral set at 1.5 degrees. I must also note that I have cut the root ends of the main and rear spars at an angle of 1.5 degrees to allow for the dihedral as well. The leading and trailing edges will butt up to this rib, and the spars will only contact the rib at their upper edges at the root end due to the cutouts. Shimming may be required to make proper contact with the spars, but shouldn't be a problem.
Hope all this makes sense.
Ed and John:
What I did is make the bottom cutouts for wing attach bolts as did Ed in a blank of 1/4" ply. Then I clamped this to the end rib of the center section with its bottom edge flush to the bottom of the center section. I simply traced the outline of the center section onto this blank, placing a piece if 1/16 ply on the top of the center section end rib to simulate the thickness of the tank.
When I join this rib to the leading and trailing edges of the wing panel, I will then bolt the spars to the center section as Ed did and raise the wing panel up to the designed 1.5 degrees. I'll space off the end rib from the center section about 1/8" at the same time. Doing all this will result in the end rib of the wing panel being parallel to that of the center section, with the wing panel dihedral set at 1.5 degrees. I must also note that I have cut the root ends of the main and rear spars at an angle of 1.5 degrees to allow for the dihedral as well. The leading and trailing edges will butt up to this rib, and the spars will only contact the rib at their upper edges at the root end due to the cutouts. Shimming may be required to make proper contact with the spars, but shouldn't be a problem.
Hope all this makes sense.