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The aerodynamic drag acting on a cylinder at a very low Reynolds number (Stokes flow or creeping motion) is a function of dyn
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Fo Drag force ML-lg-2 Milt M Dynamic visce nscosity Diameter & L free sheam v velocity Fo = f( di, au LTH Fo= K ua do uc MeltPlease dear thumpsup for the answer. Thank you.

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