We can calculate the Reynolds number as (see https://en.wikipedia.org/wiki/Reynolds_number)
"\\mathrm{Re} = \\dfrac{\\rho v D}{\\mu} = \\dfrac{900\\,\\mathrm{kg\/m^3}\\cdot2.5\\,\\mathrm{m\/s}\\cdot0.020\\,\\mathrm{m}}{0.4\\,\\mathrm{Ns\/m^2}} = 112.5."
112.5 < 2000, therefore the flow is laminar.
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