Chapter 6: Problem 2
The velocity in a certain flow field is given by the equation $$\mathbf{v}=x \hat{\mathbf{i}}+x^{2} z \hat{\mathbf{j}}+y z \hat{\mathbf{k}}$$ Determine the expressions for the three rectangular components of acceleration.
Chapter 6: Problem 2
The velocity in a certain flow field is given by the equation $$\mathbf{v}=x \hat{\mathbf{i}}+x^{2} z \hat{\mathbf{j}}+y z \hat{\mathbf{k}}$$ Determine the expressions for the three rectangular components of acceleration.
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Get started for freeDetermine the shearing stress for an incompressible Newtonian fluid with a velocity distribution of \(\mathbf{V}=\left(3 x y^{2}-4 x^{3}\right) \mathbf{i}+\) \(\left(12 x^{2} y-y^{3}\right) \mathbf{j}\).
Blood flows at volume rate \(Q\) in a circular tube of radius \(R\). The blood cells concentrate and flow near the center of the tube. while the cell-free fluid (plasma) flows in the outer region. The center core of radius \(R_{c}\) has a viscosity \(\mu_{c}\) and the plasma has a viscosity \(\mu_{p}\). Assume laminar, fully developed flow for both the core and plasma flows and show that an "apparent" viscosity is defined by $$\mu_{\mathrm{app}}=\frac{\pi R^{4} \Delta p}{8 L Q}$$ is given by $$\mu_{\mathrm{app}}=\frac{\mu_{p}}{1-\left(R_{c} / R\right)^{4}\left(1-\mu_{p} / \mu_{c}\right)}$$
In Section \(6.3,\) we derived the differential equation(s) of linear momentum by considering the motion of a fluid element. Derive the linear momentum equation(s) by considering a small control volume, like we did for the continuity equation in Section 6.2.
For each of the following stream functions, with units of \(\mathrm{m}^{2} / \mathrm{s},\) determine the magnitude and the angle the velocity vector makes with the \(x\) axis at \(x=1 \mathrm{m}, y=2 \mathrm{m} .\) Locate any stagnation points in the flow field. (a) \(\psi=x y\) (b) \(\psi=-2 x^{2}+y\)
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.
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