The quick way out!
Hello Ivan,
Interesting. Yes, I understand your arguments. In this case it was a matter of fitting a spar which was half the width of a slanted aft-cabin roof-side component-part with vertices matching the vertical aft cabin wall. As it was half the width, halfway along a slanted edge, the position was 0.005 ft off in any direction.
3 extra matching vertices, 1 on the spar, 1 on the aft cabin wall and also 1 on the slanted cabin-roof side would have definitely served too, but then I would have had to run the SCASM processes for the 2 Jeeps again and with so many entries it seemed too much work, so the 227 instead of 228 SCASM adjustment was the quickest way. In effect, I thought I´d solved that hairline crack in the aft canopy before SCASMing the 2 planes, but it was still there, only smaller!
Actually, on the same canopy frame spar, in a different position, I had already successfully joined a second, thinner slanted spar that was also 0.005 ft off, and in this case an extra vertex did the trick perfectly (without extra triangulation - for which there are no parts left over anyway on these planes!).
I realize that the inside virtual view can use different parts to those of the outside view, but in this case, the hairline crack coincided in both cases, only that in the V-cockpit Chase-view it was much more noticeable as it was much closer, and the same part from the outside was also still slightly defective, so this way it was also the easiest way to kill both problems at the same time.
The narrower canopy frame you mention: Then that would be fitted in such a way that it wouln´t need to match any of the other parts, of course, as it would overlap and cover any gaps. Possibly that would also give a better feeling for a small, cramped cockpit like in this case, without such an ample "bridge"-like sensation! I´ll take that into account next time!
Cheers,
Aleatorylamp