$(A)$ $\frac{\left|\overrightarrow{ V }_{ P }\right|}{\left|\overrightarrow{ V }_{ Q }\right|}=\frac{\eta_1}{\eta_2}$ $(B)$ $\frac{\left|\overrightarrow{ V }_{ P }\right|}{\left|\overrightarrow{ V }_{ Q }\right|}=\frac{\eta_2}{\eta_1}$
$(C)$ $\overrightarrow{ V }_{ P } \cdot \overrightarrow{ V }_{ Q } > 0$ $(D)$ $\overrightarrow{ V }_{ P } \cdot \overrightarrow{ V }_{ Q } < 0$
From equilibrium, $\sigma_1+\sigma_2=\rho_1+\rho_2$
$V _{ p }=\frac{2}{9}\left(\frac{\rho_1-\sigma_2}{\eta_2}\right) g \text { and } V _{ Q }=\frac{2}{9}\left(\frac{\rho_2-\sigma_1}{\eta_1}\right) g$
So, $\frac{\left|\overrightarrow{ V }_{ P }\right|}{\left|\overrightarrow{ V }_{ Q }\right|}=\frac{\eta_1}{\eta_2}$ and $\overrightarrow{ V }_{ P } \cdot \overrightarrow{ V }_{ Q }<0$

(ignore viscosity of air)