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Kelly Troyer wrote:
Jim and Ernest,
Jim I also thank you for your valid concern and input........The NACA report
that has provided much of the design info for our "in wing" cooling systems has
reported a slight increase in lift with certain outlet positions.......Believed to be the result of reattachment of the boundry layer after going turbulent aft of the outlet.....
In case you want to review it, the report Kelly refers to can be found at:
http://ernest.isa-geek.org/Delta/Library/naca-report-WingRadiators.pdf
And while I was retrieving that one for the upteenth time, I found another that I hadn't read before:
http://ernest.isa-geek.org/Delta/Library/naca-report-WingDuctCooling.pdf
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,|"|"|, Ernest Christley |
----===<{{(oQo)}}>===---- Dyke Delta Builder |
o| d |o www.ernest.isa-geek.org |
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