Unit Reynolds number, Mach number and pressure gradient effects on laminar–turbulent transition in two-dimensional boundary layers
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DOI: 10.1007/s00348-018-2538-8
Abstract: The influence of unit Reynolds number ($$Re_1=17.5\times 10^{6}$$Re1=17.5×106–$$80\times 10^{6}\,\text {m}^{-1}$$80×106m-1), Mach number ($$M= 0.35$$M=0.35–0.77) and incompressible shape factor ($$H_{12} = 2.50$$H12=2.50–2.66) on laminar–turbulent boundary layer transition was systematically investigated in the Cryogenic Ludwieg-Tube Göttingen (DNW-KRG).… read more here.
Keywords: transition; reynolds number; unit reynolds; number ... See more keywords