PaulS
Well-Known Member
I have attached a foil ".dat" file.
I would like an independent evaluation as a foil and as a wing with a 5'5" (1651mm) chord anda 30' (9144mm) span.
all you have to do is to rename it from Crow3.txt to Crow3.dat
my evaluation has shown that at14 degree alpha the flow at the trailing edge reattaches preventing stall through at least 16 degrees alpha.
I would be interested in the software you use and the conditions.
I tried to upload the screen shot of the test at 16 degrees but the file is too large - I will resize it and see if it is still readable.
I would like an independent evaluation as a foil and as a wing with a 5'5" (1651mm) chord anda 30' (9144mm) span.
all you have to do is to rename it from Crow3.txt to Crow3.dat
my evaluation has shown that at14 degree alpha the flow at the trailing edge reattaches preventing stall through at least 16 degrees alpha.
I would be interested in the software you use and the conditions.
I tried to upload the screen shot of the test at 16 degrees but the file is too large - I will resize it and see if it is still readable.