Chapter 6: Problem 110
Consider the flow field presented by the potential function $\phi=x^{5}-10 x^{3} y^{2}+5 x y^{4}-x^{2}+y^{2} .$ Verify that this is an incompressible flow, and obtain the corresponding stream function.
/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none}
Learning Materials
Features
Discover
Chapter 6: Problem 110
Consider the flow field presented by the potential function $\phi=x^{5}-10 x^{3} y^{2}+5 x y^{4}-x^{2}+y^{2} .$ Verify that this is an incompressible flow, and obtain the corresponding stream function.
All the tools & learning materials you need for study success - in one app.
Get started for free
An incompressible liquid with a density of \(1250 \mathrm{kg} / \mathrm{m}^{3}\) and negligible viscosity flows steadily through a horizontal pipe of constant diameter. In a porous section of length \(L=\) \(5 \mathrm{m},\) liquid is removed at a constant rate per unit length so that the uniform axial velocity in the pipe is \(u(x)=U(1-x / L)\) where \(U=15 \mathrm{m} / \mathrm{s}\). Develop expressions for and plot the pressure gradient along the centerline. Evaluate the outlet pressure if the pressure at the inlet to the porous section is \(100 \mathrm{kPa}(\text { gage })\)
An old magic trick uses an empty thread spool and a playing card. The playing card is placed against the bottom of the spool. Contrary to intuition, when one blows downward through the central hole in the spool, the card is not blown away. Instead it is "sucked" up against the spool. Explain.
In a two-dimensional frictionless, incompressible \(\left(\rho=1500 \mathrm{kg} / \mathrm{m}^{3}\right)\) flow, the velocity field in meters per second is given by \(\vec{V}=(A x+B y) \hat{i}+(B x-A y) \hat{j} ;\) the coordinates are measured in meters, and \(A=4 \mathrm{s}^{-1}\) and \(B=2 \mathrm{s}^{-1}\). The pressure is \(p_{0}=200 \mathrm{kPa}\) at point \((x, y)=(0,0) .\) Obtain an expression for the pressure field, \(p(x, y)\) in terms of \(p_{0}, A,\) and \(B,\) and evaluate at point \((x, y)=(2,2)\)
Steady, frictionless, and incompressible flow from left to right over a stationary circular cylinder, of radius \(a,\) is represented by the velocity field \\[ \vec{V}=U\left[1-\left(\frac{a}{r}\right)^{2}\right] \cos \theta \hat{e}_{r}-U\left[1+\left(\frac{a}{r}\right)^{2}\right] \sin \theta \hat{e}_{\theta} \\] Obtain an expression for the pressure distribution along the streamline forming the cylinder surface, \(r=a\). Determine the locations where the static pressure on the cylinder is equal to the freestream static pressure.
A flow nozzle is a device for measuring the flow rate in a pipe. This particular nozzle is to be used to measure low-speed air flow for which compressibility may be neglected. During operation, the pressures \(p_{1}\) and \(p_{2}\) are recorded, as well as upstream temperature, \(T_{1}\). Find the mass flow rate in terms of \(\Delta p=p_{2}-p_{1}\) and \(T_{1},\) the gas constant for air, and device diameters \(D_{1}\) and \(D_{2}\). Assume the flow is frictionless. Will the actual flow be more or less than this predicted flow? Why?
What do you think about this solution?
We value your feedback to improve our textbook solutions.