Hi all,
Glad there's been an eventual acknowledgement / realisation of the taper issue. As myself, and, more recently Bo have said, once seen impossible not to see. My original post on the other forum explained the whole thing completely, but as mentioned, generated little response. Still waiting for my 'Whiz Kid' with these modern electronic boxes to show me how to resize flies to 'postable' size.
When she gets round to it I'll post the photos of my 1/72nd Roden DIII which incorporated the mods, also photos of notes I made back in 1988 which explain the whole thing in complete detail. These are 'gathering dust' stapled to the back cover of the original Datafile, hey, was it really twenty six years ago I made those notes?, By Gum, I was but a slip of a boy!.
The notes will explain everything raised and make clear what needs to be done to the tips (or not done - if anyone wants to build from the box that's fine, depends what the individual wants)
Rag, briefly, the taper, or 'droop', starts from the second rib out from the aileron root, the red line in your photo, there is also, as previously mentioned 'upsweep' on the lower surface commencing from same point.
Best thing for me to do here is to post stuff mentioned above which explain it all a lot better than I have time to do now, stand by on that. Interestingly it is possible to come up with 'guesstimated' aerofoil co-ordinates for the tips using various datums, we of course know the co-ordinates for the constant areas of upper and lower wings. On the notes I hope to post mention is made also of aileron geometry and how this tied in. If anyone has either the original DIII Datafile or the later Issue take a look at the pic of 4184/17 on page 21 in the original issue or page 24 in the later issue. Hold page obliquely and sight along top surfaces of upper surfaces of front and rear spars (upper surface of front spar only visible in later issue) this illustrates commencement points, this is only 'straight' on the spar surface itself and on the aileron false spar and aileron leading edge. The 'staightness' was eased very slightly on the rib profile, a very slight curve to the tip, 'almost straight'. Also look on same photos for corresponding 'upsweep' on lower surface. Phew. Stand by for posts and keep taking tablets all,
Cheers, Al.