Quote:
Originally Posted by Kevin Horton
Bob,
Have you ever tested the exact same configuration multiple times on different days to see how much scatter there is in the results?
I'm betting you would find a kt or two of scatter, which means that perhaps you need more than one test point on one flight to decide whether a change has given a small speed increase or not.
Why not fly a couple more tests on different days with your current configuration?
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Any credible test program would need that. I want to try to see what I can get out of this strictly for the speed of this airplane so I am motivated a little differently. Test 14 in this series was a little disappointing - I am starting to visualize a combination of forces at play and I thought the relief of the cutouts in the cover would have a greater positive effect than I saw.
With the test rsults sorted by speed I think I have a better direction for the next step:
Here are some things I think are true from the test results so far:
The bump is better than no bump
Restriction in the outlet path can slow the plane down
There are a lot more things that I suspect but I do not know so I will just stew on those as I proceed. I am going to go back to test configuration #10 and re-fly that. I can rationalize that it is the best configuration tested so far just by direct observation but even with a test method error margin of 2kts it is still well within the top group tested.
Test configuration 7 and the related long cover configuration that was not tested but appeared to perform well but was shattered are also on my mind. I am not convinced that the long tail bump is better than the symetrical bump and I am not convinced that there is nothing to be gained from some form of cover - yet.
For now I'll re-fly test configuration #10 which I hope will not disappoint me. If test #10 results are validated I can focus on optimizing that configuration for a while.
Bob Axsom