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ael65
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Lets assume that vacuum empty cylinder has a spinning top. Rotational speed at circumference is V. Cylinder axis is oriented verticaly. Cylinder is surranded by air at athmospheric pressure and weights slightly more then displaced air.
According to Bernoulli principle there should be pressure differential dp between top and bottom becuase of fluid speed difference. Bottom is stationary Vb=0, Average speed of top is Vt = 2/3*V (if I calculated correctly). This means that dp = <air density> * Vt * Vt / 2.
Question: will cylinder fly if top spins fast enough ?
-al
According to Bernoulli principle there should be pressure differential dp between top and bottom becuase of fluid speed difference. Bottom is stationary Vb=0, Average speed of top is Vt = 2/3*V (if I calculated correctly). This means that dp = <air density> * Vt * Vt / 2.
Question: will cylinder fly if top spins fast enough ?
-al