(a)
The characteristic scale for v, y-component of velocity.
Answer to Problem 27P
The characteristic scale for v, y-component of velocity is
Explanation of Solution
First, we need to use continuity equation for velocity component.
From continuity equation,
We have,
Now, to obtain order of magnitude. We need to use characteristic scale separately.
We have,
Now, characteristic scale v is,
(b)
The order of magnitude of inertial term to that of viscous and pressure term.
Answer to Problem 27P
The characteristic scale for v, y-component of velocity is
Explanation of Solution
First, we need to use momentum of x-component.
As we know that the flow is carried out in two-dimensional, so the z component will be zero.
Now, to obtain order of magnitude. We need to use characteristic scale separately.
We have,
Now,
The second term of viscosity is very smaller as compared to the second viscous term. So, we neglect this term (ho<
Now, we need to multiply all the order of magnitude with a factor of
Now,
We can see that the order of magnitude consists a factor of
(c)
If the value of Reynolds number is less than 1 and (ho<
Explanation of Solution
First, we need to use momentum of x-component.
As we know that the flow is carried out in two-dimensional, so the z component will be zero.
Now, to obtain order of magnitude. We need to use characteristic scale separately.
We have,
Now,
The second term of viscosity is very smaller as compared to the second viscous term. So, we neglect this term. (ho<
Now,
We can see that the order of magnitude consists a factor of
Want to see more full solutions like this?
Chapter 10 Solutions
FLUID MECHANICS FUND. (LL)-W/ACCESS
- the differential equation for conservation of mass, the continuity equation. In cylindrical coordinates, and for steady flow, 1/ r ∂(rur) /∂r + 1/ r ∂u? /∂? + ∂uz /∂z = 0 Write the primary dimensions of each additive term in the equation, and verify that the equation is dimensionally homogeneous. Show all your work.arrow_forwardfind mach and reynolds number and write out N-S eqnsarrow_forwardPlease answer with detailarrow_forward
- Compute the b Am? when the lower plate Steady skte momentum Flex Ey> momentum Ilex ty Velscity v in the Figure beloo is 0.804n/s s the pasitive X-directan, the Separation Y s o 304mm, md the fluid viscosity N is o7cP Naly) Longe t Final uelociny distribution in teady Flowarrow_forwardMott ." cometer, which we can analyze later in Chap. 7. A small ball of diameter D and density p, falls through a tube of test liquid (p. µ). The fall velocity V is calculated by the time to fall a measured distance. The formula for calculating the viscosity of the fluid is discusses a simple falling-ball vis- (Po – p)gD² 18 V This result is limited by the requirement that the Reynolds number (pVD/u) be less than 1.0. Suppose a steel ball (SG = 7.87) of diameter 2.2 mm falls in SAE 25W oil (SG = 0.88) at 20°C. The measured fall velocity is 8.4 cm/s. (a) What is the viscosity of the oil, in kg/m-s? (b) Is the Reynolds num- ber small enough for a valid estimate?arrow_forward1. The Stokes-Oseen formula for drag force Fon a sphere of diameter D in a fluid stream of low velocity V, density p, and viscosity u is: 9T F = 3TuDV + 16PD? Is this formula dimensionally homogenous? 2. The efficiency n of a pump is defined as the (dimensionless) ratio of the power required to drive a pump: QAp input power Where Q is the volume rate of flow and Ap is the pressure rise produced by the pump. Suppose that a certain pump develops a pressure of Ibf/in? (1ft = 12 in) when its flow rate is 40 L/s (1L =0.001 m). If the input power is 16hp (1hp = 760 W), what is the efficiency?arrow_forward
- The x-component of the Navier-Stokes equations is given below. Convert it to dimensionless form using a velocity scale U, a length scale I, and a pressure scale P. du at du du du +u+v+w. = ax dy az 1 op μdu du du + + pax² ay ² a=² paxarrow_forwardFind the vorticity of the fluid motion for the given velocity com- ponents. KINEMATICS OF FLUIDS (a) u A(x + y), v = - A(x + y) (b) u = 2Axz, (c) u Ay²+ By + C, v = A(c² + x² - z²) 1)=0arrow_forwardV u-v Question 4: Consider fully developed Couette flow - flow between two infinite parallel plates separated by distance h, with the top plate moving and the bottom plate stationary as illustrated. The flow is steady, incompressible, and two dimensional in the xy-plane. The velocity field is given by V = (u,v) = (V y/h)ỉ + 0ỷ, Generate an expression for stream function Yalong the vertical dashed line in the figure. For convenience, 4= 0 along the bottom wall of the channel. What is the value of Y along the top wall?arrow_forward
- FLUID MECHANICSarrow_forwardQ1:: Explain all the terms of the Continuity Equation and their physical meanings with the help of examples.arrow_forwardTwo infinite plates a distance h apart are parallel to the xzplane with the upper plate moving at speed V, as inFig. There is a fluid of viscosity μ and constant pressurebetween the plates. Neglecting gravity and assumingincompressible turbulent flow u(y) between the plates, usethe logarithmic law and appropriate boundary conditions toderive a formula for dimensionless wall shear stress versusdimensionless plate velocity. Sketch a typical shape of theprofile u(y).arrow_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