I am trying to understand what is shown in this book (Applied hydro and aeromechanics), page 187

The velocity induced at a given point on a parallel plane by a vortex segment of length $b$, and strength $\Gamma$ is shown to be,

$v_1 = \frac{\Gamma b \, sin \, \alpha}{4 \pi R^2}$

Can anyone please show the steps on arriving this formula by applying Biot-Savart law ?

  • $\begingroup$ Please don't double post messages. $\endgroup$ – DeltaLima Feb 21 '17 at 10:56
  • $\begingroup$ Meta post explaining why not to double post is here $\endgroup$ – Notts90 Feb 21 '17 at 11:34
  • $\begingroup$ I have answered this on physics.SE. $\endgroup$ – Peter Schilling Jul 13 '17 at 21:48

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