Chapter 6: Problem 25
By considering the rotational equilibrium of a fluid mass element, show that \(\tau_{x y}=\tau_{y x}\).
Chapter 6: Problem 25
By considering the rotational equilibrium of a fluid mass element, show that \(\tau_{x y}=\tau_{y x}\).
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Get started for freeA Bingham plastic is a fluid in which the stress \(\tau\) is related to the rate of strain \(d u / d y\) by $$\tau=\tau_{0}+\mu\left(\frac{d u}{d y}\right)$$ where \(\tau_{0}\) and \(\mu\) are constants. Consider the flow of a Eingham plastic between two fixed, horizontal, infinitely wide, flat plates. For fully developed flow with \(d u / d x=0\) and \(d p / d x\) constant. find \(u(y)\).
The flow in the impeller of a centrifugal pump is modeled by the superposition of a source and a free vortex. The impeller has an outer diameter of \(0.5 \mathrm{m}\) and an inner diameter of \(0.3 \mathrm{m}\). At the outlet from the impeller, the flowing water has the following velocity componeats, relative to the impeller: radial component \(2 \mathrm{m} / \mathrm{s}\) and tangential comporent \(7 \mathrm{m} / \mathrm{s}\). (a) Find the strength of the source and the vortex required to model this flow. (b) Assume that the impeller blades are shaped like the streamlines and plot an impeller blade shape. (c) Find the radial and tangential components of velocity at the inlet to the impeller.
An infinitely long, solid, vertical cylinder of radius \(R\) is located in an infinite mass of an incompressible fluid. Start with the Navier-Stokes equation in the \(\theta\) direction and derive an expression for the velocity distribution for the steady-flow case in which the cylinder is rotating about a fixed axis with a constant angular velocity \(\omega\). You need not consider body forces. Assume that the flow is axisymmetric and the fluid is at rest at infinity.
Two immiscible, incompressible, viscous fluids having the same densities but different viscosities are contained between two infinite, horizontal, parallel plates (Fig. \(P 6.80\) ). The bottom plate is fixed, and the upper plate moves with a constant velocity \(U\) Determine the velocity at the interface. Express your answer in terms of \(U, \mu_{1},\) and \(\mu_{2}\). The mo:ion of the fluid is caused entirely by the movement of the upper plate; that is, there is no pressure gradient in the \(x\) direction. The fluid velocity and shearing stress are continuous across the interface between the two fluids. Assume laminar flow:
A liquid of constant density \(\rho\) and constant viscosity \(\mu\) flows down a wide, long inclined flat plate. The plate makes an angle \(\theta\) with the horizontal. The velocity components do not change in the direction of the plate, and the fluid depth, \(h,\) normal to the plate is constant. There is negligible shear stress by the air on the fluid. Find the velocity profile \(u(y),\) where \(u\) is the velocity parallel to the plate and \(y\) is measured perpendicular to the plate. Write an expression for the volume flow rate per unit width of the plate.
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