posted 12-29- 02:52 PM
Yep, I'll post a full tutorial to the best of my ability - w/screen shots, etc. If people start getting into airfoils I think we will see a big step forward for FM.From what I know Pete, this is the way it works:
1. Download the wing extractor app on Tail's website.
2. Load an existing airfoil that most closely matches your plane. The SDOE standard airfoils come with the wing extractor, or unbig the par file and look in the media/aircraft/airfoils folder.
3. Update the data - more on this below
4. Save the airfoil to the media/aircraft/airfoils directory. Name it to match your plane or whatever.
5. Open this new airfoil.sm file in a binary editor - you can download one from www.shareware.com or whatever.
6. Edit all occurences of the name of your airfoil. In my case I named my airfoil SE5a0.sm - so I replaced the 4 occurences of this, stuff like FW190.sm in the media path and FW190foil, FW190foilup, FW190foildoen - all became SE5a0.sm, SE5afoil, etc. Now save this file again.
7. Open up startup.ppf in the media folder. You must unbig a parfile to get this, or someone can send you one - I'll post it at my site. Now add your airfoil to the list of airfoils. I added "Se5a0foil"
8. Now open your plane in OPS and look at the property for any air object - change the foil to be your airfoil, in my case, "Se5a0foil". Save the plane
9. Try it! I bet is sucks 
OK, the only hard part here is editing the airfoil data. The app still confuses me. Anyway, you will see a chart. The x axis is AOA - from 180 degress neg om the left to 180 degrees plu on the left. The Y axis is the cooficiant - green line of co. of drag, the red line is the co. of lift. There are other lines - but I dont understand how they effect FM - like Cooefficiant of Momentum.
Here is my trouble: how to best edit the curve? I though I would be clicking and draging points - no! Instead you choose a range from the X axis (00 - 50?) and a "left multiply" and "right multiple" - this will alter the curve in that AOA range - tricky work to get what you want. Also it is hard because you don't see AOA in degress labeled on the chart. 25 is 0 degrees angle of attack.
I'm sure using the chart is hard for me only because I don't understand the problems related to airfoil data editing.
Anyway, for my SE5a I simply increased the drag coef. at AOA at about 8 degrees and above to try to get more speed bleeding when maneuvering. It worked, but no my SE5a is dead at low alt, and flys super good at 10,000 feet
- slight turns at low alt cause the speed to drop real fast - at high alt (10,000 feet) I can turn sharp circles forever with not enough drag to slow the plane down.
My guess is that my prop is to efficiant at high alt or something. Anyone have any prop tips? 
More later...
------------------
-Sv =FC=
WWI in SDOE!