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Generally, the interceptor height should not be higher than 60percentt of boundary layer thickness at transom.
The boundary layer thickness at the position where the upstream array of the actuators locates is δ = 2.11 mm.
The turbulent boundary layer thickness at which the cylindrical structure was placed varied from 26 120 mm.
The present work achieves the recommended contraction ratio, maximum uniformity at the working section mid-plane, without separation, no Gortler vortices in the contraction, and minimizing the boundary layer thickness at entrance to the working section.
Each fence model was located in uniform flow whose boundary layer thickness at the fence location was about 0.1 of the fence height (H).
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The results of this study show that among all effective variables, the boundary layer thickness (h) at the stern (where the interceptor is installed), is far more important than, some other particular parameter, on interceptor performance and should be taken into account in estimating the interceptor height (d) and span (s).
The results reveal that the boundary layer thickness and flow velocity increase at high Richardson number for both porous and clear channels.
This is because with an increase in nanoparticles volume fraction, the thermal conductivity of the nanofluid increases, which reduces the thermal boundary layer thickness and the temperature gradient at the wall.
The effects of lateral mass flux, Rayleigh number, wall inclination angle, wall temperature distribution, porosity and conductivity variation of the porous material on boundary layer thickness and heat-transfer characteristics at the surface are presented.
The boundary layer thickness, velocity profile and transition region at varying transverse distances from the plate centre line are determined.
The growth in thermal boundary layer thickness is responsible for the lesser temperature gradients at the surface of the tube which results lower convective heat transfer coefficient accordingly.
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