![]() |
| If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|||||||
|
|
Thread Tools | Display Modes |
|
#34
|
|||
|
|||
|
Andy, see comments below:
I would think that using rate of change of curvature (or absolute curvature) to estimate the thickness of the overall airfoil would be really challenging. It's kind of like using an accelerometer (or variometer) to estimate your altitude - it's possible if you're really good at integrating the values, but you need very accurate measurements to keep the integrated sum from drifting pretty significantly. You're right. It's probably poor for profiling the whole wing. But it worked reasonably well in picking up flaws that were bigger than the wave gauge but substantially smaller than the chord. If I'd known I had a significant problem when I started, I'd probably have tried to make templates. But by the time I finally figured out what the problem was, I felt like I could go ahead with the dial gauge. Frankly, an experienced tuner like Hank Nixon would pick up that kind of problem simply by running his hand over the wing! Can anyone tell me if it really matters if the overall thickness of the wing is off by a few thousandths. This is the difference between sanding down to the spar wave and building up gelcoat in the spar wave. I think most people sand down if they can and build up if they have to. The main reason we sprayed to build up was that this was the second time the glider was in for sanding and there simply wasn't enough gel coat over the leading and trailing edges of the spar cap; I was already seeing dark spots. You're right about overall thickness. The later LS-3a wings (I had an earlier "3") allegedly were as much as 2% thicker than spec in some places. That's a half inch on, say, a 24" chord!!! From memory, Dick Johnson found similar things on his PIK-20 and just extrapolated the airfoil for thicker sections since he had the coordinates for both 15% and 17% sections. I thought the main objective of reprofiling these days was to remove surface waviness - but this adds a new level of complexity - should I even worry about it? 9B I sanded/contoured my LS-3 three times in the 12 years I owned it in addition to extensive sealing and other tuning. The only thing I've done to my ASW-24 over the past 12 years is add winglets. One reason is that the '24 wing is amazingly stable over time (maybe one of the best composite gliders ever). The other reason is that I was single when I owned the '3 and with a 9 to 5 job. Now I'm married with two children, and average 60 hour weeks! If you're really worried about it, I recommend selling your '27 and buying a PW-5. ![]() Chip Bearden |
| Thread Tools | |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| ANG Woman Wing Commander Doesn't See Herself as Pioneer, By Master Sgt. Bob Haskell | Otis Willie | Military Aviation | 0 | March 18th 04 09:40 PM |
| Wing tip stalls | mat Redsell | Soaring | 5 | March 13th 04 06:07 PM |
| Props and Wing Warping... was soaring vs. flaping | Wright1902Glider | Home Built | 0 | September 29th 03 04:40 PM |
| Can someone explain wing loading? | Frederick Wilson | Home Built | 4 | September 10th 03 03:33 AM |
| An Affordable Homebrue 60 in DS machine | Grant | Soaring | 0 | August 8th 03 04:52 AM |