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Behavior of oscillatory tube flow at liquid-gas interfaces

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Figure

FIG. 1. Experimental setup (lengths ratios are not in true scale).
TABLE I. Experimental settings and values of the characteristic flow numbers at the interface of oscillatory tube flow.
FIG. 2. Velocity vectors below the free surface for f = 10 Hz and A = 1.00 mm, (a) particle path images of the streamingmotion as superposition of particle images for 20 subsequent periods, (b) velocity field obtained from cross-correlation,(c) typical vortex pattern (schematically).
FIG. 4. Superposed particle images for 20 subsequent periods at ffree surface, = 10 Hz, (a) liquid-wall interface, ϵ = 0.08, α = 8.5, (b) ϵ = 0.08, α = 8.5, (c) free surface, ϵ = 0.08, lower viscosity (α = 12.3), (d) liquid-wall interface, ϵ = 0.3, α =8.5, (e) free surface, ϵ = 0.3, α = 8.5, (f) free surface, ϵ = 0.3, lower viscosity (α = 12.3).
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