The drag of an airfoil at zero angle of attack is a function of density, viscosity, and velocity, in addition to a length parameter
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For a rectangular duct of cross-section as shown:
where AR (
A
spect
R
atio) =
Darcy
Friction Factor
with (ii)
For a pipe
of length L and diameter D
(Darcy-Weisbach Equation)
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