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 horizontal pipe
,
and
for a length
, L,
of the pipe
,
(Hagen-Poiseuille equation)
but
[
Darcy-Weisbach Equation]
f
Re
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(Hagen-Poiseuille equation)
Darcy-Weisbach Equation]
