/*! 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} Problem 25 A velocity field is given by \(\... [FREE SOLUTION] | 91Ó°ÊÓ

91Ó°ÊÓ

A velocity field is given by \(\vec{V}=\left[A x^{3}+B x y^{2}\right] \hat{i}+\) \(\left[A y^{3}+B x^{2} y\right] \hat{j} ; A=0.2 \mathrm{m}^{-2} \cdot \mathrm{s}^{-1}, B\) is a constant, and the coordinates are measured in meters. Determine the value and units for \(B\) if this velocity field is to represent an incompressible flow. Calculate the acceleration of a fluid particle at point \((x, y)=(2,1) .\) Evaluate the component of particle acceleration normal to the velocity vector at this point.

Short Answer

Expert verified
The constant B should be -0.6 m^{-2}s^{-1} in order for the velocity field to represent an incompressible flow. The acceleration of a fluid particle at the point (2,1) is 0.8 i - 1.6 j m^{-1}s^{-1}, and the acceleration component normal to the velocity vector at this point is 0 m/s^{2}.

Step by step solution

01

Determine the value of B

Calculate the derivative of the velocity components with respect to their respective variables. Using \( \nabla \cdot \vec{V} = \frac{ \partial V_x }{ \partial x } + \frac{ \partial V_y }{ \partial y } = 0 \), where \( V_x = A x^{3}+B x y^{2} \) and \( V_y = A y^{3}+B x^{2} y \). After differentiation and simplifying, the equation will be \( 3Ax^{2} + By^{2} + 3Ay^{2} +Bx^{2} =0 \). For an incompressible flow, the total divergence must be zero for all (x, y). Therefore, \( 3A + B = 0 \), which implies \( B = -3A = -3(0.2 \, m^{-2}s^{-1}) = -0.6 \, m^{-2}s^{-1} \). This is the value and units for B in order for the velocity field to represent an incompressible flow.
02

Calculate the acceleration of a fluid particle

The acceleration of a particle in the flow is given by the time derivative of the velocity vector. The velocity vector does not vary with time explicitly. However, since the position of the particle changes with time, we need to take the convective derivative which gives the path-dependent change, \( a = \frac {d \vec{V}} {dt} = \frac {\partial \vec{V}} {\partial t} + \vec{V} \cdot \nabla \vec{V} \). With given values of \(x = 2, y = 1\), we find \( a_x = \vec{V} \cdot \nabla (\vec{V}_x) = (A x^{3}+B x y^{2}) \cdot (3Ax^{2}+2By) = (0.2*8 - 0.6*4) = 0.8 \, m^{-1}s^{-1}\) and \( a_y = \vec{V} \cdot \nabla (\vec{V}_y) = (A y^{3}+B x^{2} y) \cdot (3Ay^{2}+2Bx) = (0.2*1 - 0.6*4) = -1.6 \, m^{-1}s^{-1}\). Hence, acceleration \( a = a_x \hat{i} + a_y \hat{j} = 0.8 \hat{i} - 1.6 \hat{j} m^{-1}s^{-1} \).
03

Evaluate the component of particle acceleration normal to the velocity vector

The normal component of acceleration is obtained by first calculating the magnitude (speed) of the velocity vector at the given point. Then, find the dot product of acceleration and velocity vectors and subtract it from the total acceleration. Evaluate at \( (x, y) = (2, 1) \). The speed \( V_s = \sqrt{V_x^{2} + V_y^{2}} = \sqrt{(0.2*8)^{2} + (-1.2*2)^{2}} = 2.24 m/s \). The tangential component of acceleration \( a_t = \vec{a} \cdot \frac{\vec{V}}{V_s} = (0.8 \hat{i} - 1.6 \hat{j})\cdot (\frac{1.6\hat{i} - 2.4\hat{j}}{2.24}) = 1.28 m/s^{2} \). Hence, normal component \( a_n = \sqrt{a^{2} - a_t^{2}} = \sqrt{1^{2} - 1.28^{2}} = 0 m/s^{2} \).

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with 91Ó°ÊÓ!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

The stream function of a flow field is \(\psi=A x^{2} y-B y^{3},\) where \(A=1 \mathrm{m}^{-1} \cdot \mathrm{s}^{-1}, B=\frac{1}{3} \mathrm{m}^{-1} \cdot \mathrm{s}^{-1},\) and the coordinates are measured in meters. Find an expression for the velocity potential.

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.

Consider frictionless, incompressible flow of air over the wing of an airplane flying at \(200 \mathrm{km} / \mathrm{hr}\). The air approaching the wing is at 65 kPa and \(-10^{\circ} \mathrm{C}\). At a certain point in the flow, the pressure is 60 kPa. Calculate the speed of the air relative to the wing at this point and the absolute air speed.

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 \((x, y)=(2,2)\)

Water flows in a circular duct. At one section the diameter is \(0.3 \mathrm{m}\), the static pressure is \(260 \mathrm{kPa}\) (gage), the velocity is \(3 \mathrm{m} / \mathrm{s},\) and the elevation is \(10 \mathrm{m}\) above ground level. At a section downstream at ground level, the duct diameter is \(0.15 \mathrm{m}\) Find the gage pressure at the downstream section if frictional effects may be neglected.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.