I've been installing rib "pillars" to prevent C-Tube wings from crushing when building wings in my Lost-Foam system for more than 20 years. In that system we use weights on top of the top cradle piece to hold the molded shells in place while the glue dries. Tried doing that without the pillars and the result was a very thin (ahem) wing...
Another advantage of the pillars on airplanes otherwise lacking shear webs is that it keeps the ribs from splitting chordwise from shear in the spars. I recently had the, uh, opportunity to see the inside of the Skyray wing (balsa version). It is a C-tube with 1/8x1/2 10 lb spars set vertically at the high point, which means about 3/4" of unsupported balsa between the top and bottom spar slots. The spars themselves are pretty stout, but the airplane has always been prone to pulling an alarming amount of dihedral. easily visible to casual observers.
When it was disassembled, the wing that hit the ground had every single rib (3/32 4.8 lb) split from the front clearance to the rear clearance. I then stripped the other wing which had been undamaged - same thing. I am pretty well convinced that the ribs all split there on the first hard corner. Bobby's pillar would have kept it together.
The obvious question is, why no shear ribs? Thats because I wanted to be sure that the wing was flexible enough to take multiple crashes. That it did, easily 30-40 of them, with only cosmetic damage. Shear webs would have kept the dihedral out of it, but they also would likely have caused massive damage on a crash. At the least, I would expect the spars to have broken in a pancake landing, probably at the root. As it was, when the covering shattered, the spar broke right at the end of the center section sheeting - which made it to rigid.
The stock wing was light ply and spruce straight out of the kit, and it was much stiffer (and absurdly heavier) It shattered in to MANY pieces on the first significant crash and was utterly irreparable. I threw the balsa wing together in about and hour and a half, and it lasted close to 20 years and multiple crashes. Maybe surprisingly, the original airplane was something like 5-6 ounces heavier than the rebuilt model, but with the 20FP it made nearly NO difference in the performance. Right to the end, it was limited by the tail moment and elevator movement, not the wing loading. But the lighter wing was far more durable.
It may have survived this crash, too, if the Monokote had remained flexible like it was when new. As expected, in the pancake crash, it shattered like glass after sitting out in the sun on and off for 20 ish years. I wadded it up and it cracked into a million pieces. The covering on the bottom was a little stiff, but didn't crack and could not have a finger punched through it easily like the top.
Brett