Chapter 7: Problem 3
Equation \((7.1 b)\) assumes that the boundary layer on the plate is turbulent from the leading edge onward. Devise a scheme for determining the boundary layer thickness more accurately when the flow is laminar up to a point \(\mathrm{Re}_{x, \text { crit }}\) and turbulent thereafter. Apply this scheme to computation of the boundary layer thickness at \(x=1.5 \mathrm{m}\) in \(40 \mathrm{m} / \mathrm{s}\) flow of air at \(20^{\circ} \mathrm{C}\) and 1 atm past a flat plate. Compare your result with Eq. \((7.1 b) .\) Assume \(\operatorname{Re}_{x, \text { crit }}\) \(\approx 1.2 \mathrm{E} 6\).
Short Answer
Step by step solution
Define Known Values and Constants
Calculate Reynolds Number at x = 1.5 m
Determine Laminar and Turbulent Contributions
Calculate Laminar Boundary Layer Thickness
Calculate Turbulent Boundary Layer Thickness
Combine Laminar and Turbulent Thicknesses
Compare with Existing Equation (7.1b)
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