Concept explainers
Consider steady, two-dimensional, incompressible flow due to a spiraling line vortex/sink flow centered on the z-axis. Streamlines and velocity components are shown in Fig. 9-87. The velocity field is
FIGURE P9-87
The pressure field as a function
Answer to Problem 87P
The pressure field as a function
Explanation of Solution
Given information:
The flow is steady, two-dimensional and incompressible.
The velocity components are
Here,
Write the expression for continuity equation.
Here, velocity components are
Write the expression for the
Here, density is
Write the expression for the
Calculation:
Substitute
Since both sides of Equation (IV) are equal, therefore continuity equation is verified.
Substitute
Integrate Equation (V) with respect to
Here, arbitrary function is
Differentiate Equation (VI) with respect to
Substitute
Substitute
Integrate Equation (VIII) with respect to
Here, arbitrary constant is
Substitute
Conclusion:
The pressure field as a function
Want to see more full solutions like this?
Chapter 9 Solutions
Fluid Mechanics: Fundamentals and Applications
- Consider steady, two-dimensional, incompressible flow due to a spiraling line vortex/sink flow centered on the z-axis. Streamlines and velocity components are shown in Fig. The velocity field is ur = C/r and u? = K/r, where C and K are constants. Calculate the pressure as a function of r and ?.arrow_forwardExamine whether the flow is rotational or irrotational at the point (1,-1,1) for the following velocity field (V = xz³1 - 2x²yzj + 2yzªk)arrow_forwardPerform the convective on velocity vectors u in cylindrical coordinates : Du/Dtarrow_forward
- Ay j. Is this a possible case of incompres- 3.9 A velocity field is given by V= Axyi -- %3D sible flow? If yes, obtain the stream function and find the value of constant A for which the flow rate between the streamlines passing through the points (3, 3) and (3, 4) is 18 units. Axy Ans: V = 12 + C, A 7 2arrow_forwardi dont understand the questionarrow_forwardConsider two-dimensional flow in the x-y plane where we are using polar coordinatesr and O to describe the motion. We will call u the radial velocity and v the azimuthal velocity (see figure below). y u Xarrow_forward
- Consider steady, two-dimensional, incompressible flow in the xz-plane rather than in the xy-plane. Curves of constant stream function are shown in Fig. The nonzero velocity components are (u, w). Define a stream function such that flow is from right to left in the xz-plane when ? increases in the z-direction.arrow_forwardThe velocity field for a line vortex in the r?-plane is given byur = 0 u? = K / rwhere K is the line vortex strength. For the case with K = 1.5 m/s2, plot a contour plot of velocity magnitude (speed). Specifically, draw curves of constant speed V = 0.5, 1.0, 1.5, 2.0, and 2.5 m/s. Be sure to label these speeds on your plot.arrow_forwardar r rəe 6- Proof that Streamlines and equipotential lines are orthogonal to each otherarrow_forward
- A common flow encountered in practice is the crossflow of a fluid approaching a long cylinder of radius R at a free stream speed of U∞. For incompressible inviscid flow, the velocity field of the flow is given as in fig. Show that the velocity field satisfies the continuity equation, and determine the stream function corresponding to this velocity field.arrow_forwardA unifom flow field defined by y = y is superposed on =xi- vị. Determine the stream function and velocity potential for the ocombined flow [Ans. y = xy +y, = +x- 2arrow_forwardConsider fully developed Couette flow between two infinite parallel plates separated by distance h, with the top plate moving and the bottom plate stationary, as illustrated in the figure below. The flow is steady, incompressible, and two-dimensional in the XY plane. The velocity field is given by V }i = (u, v) = (v² )i +0j = V (a) Find out the acceleration field of this flow. (b) Is this flow steady? What are the u and v components of velocity? u= V² harrow_forward
- Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University PressMechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSONThermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
- Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEYMechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage LearningEngineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY