Someone argues: “Within a boundary layer the fluid slows from the free-stream speed…

PHYSICS · Multi-part · Fermi University Physics · Fluids & Continuum Physics · Viscous flow and dynamical similarity · Viscous flow and dynamical similarity

Fluid Dynamics, Ch The boundary layer: Prandtl's equations and the Blasius solution

Problem

Someone argues: “Within a boundary layer the fluid slows from the free-stream speed UU down to zero at the wall. Applying Bernoulli's theorem along the vertical line from a point at the outer edge of the layer down to the wall beneath it therefore gives pwall=pedge+12ρU2p_{\rm wall}=p_{\rm edge}+\tfrac12\rho U^2: the wall pressure exceeds the pressure at the edge of the layer by the full free-stream dynamic pressure. For air at U=12 m s−1U=12\,\mathrm{m\,s^{-1}} (ρ=1.20 kg m−3\rho=1.20\,\mathrm{kg\,m^{-3}}) that is a difference of 86.4 Pa86.4\,\mathrm{Pa}.” ((a)) Find the error in this argument. ((b)) Give an order-of-magnitude estimate of the actual pressure difference across a layer of thickness δ=5.0 mm\delta=5.0\,\mathrm{mm} on a wall of radius of curvature R=2.0 mR=2.0\,\mathrm{m}, at the same speed, and compare it with the 86.4 Pa86.4\,\mathrm{Pa} claimed above.

Browse the problem library