Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
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Converging duct flow is modeled by the steady, twodimensional velocity field V-›= (u, ? ) = (U0 + bx) i-›− byj-› where U0 is the horizontal speed at x = 0 . As vertical line segment AB moves downstream it shrinks from length ? to length ? +Δ? assketchedin.Generateananalytical expression for the change in length of the line segment, Δ? . Note that the change in length, Δ? , is negative.
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- A steady, two-dimensional velocity field in the xy-plane is given by V-›= (a + bx)i-›+ (c + dy)j-›+ 0k-›. (a) What are the primary dimensions (m, L, t, T, . . .) of coefficients a, b, c, and d? (b) What relationship between the coefficients is necessary in order for this flow to be incompressible? (c) What relationship between the coefficients is necessary in order for this flow to be irrotational? (d ) Write the strain rate tensor for this flow. (e) For the simplified case of d = −b, derive an equation for the streamlines of this flow, namely, y = function(x, a, b, c)arrow_forward(2) Consider the following fluid velocity fields: F(x,y) = (x,y), F(x,y)=(-x, y), F(x,y) = (y, 0). (a) Plot the three fields as glyphs. Which of these vector fields represent an expansion, a compression and a shear flow? (b) Calculate the divergence of the three fields V F. Can you relate the value of the divergence with the nature (compression, expansion or shear of the flow)? (c) Calculate the circulation V x F and relate it with the nature of the flow.arrow_forwardA steady, incompressible, two-dimensional velocity field is given by V-›= (u, ? ) = (2.5 − 1.6x) i-›+ (0.7 + 1.6y) j-› where the x- and y-coordinates are in meters and the magnitude of velocity is in m/s. The x-component of the acceleration vector ax is (a) 0.8y (b) −1.6x (c) 2.5x − 1.6 (d ) 2.56x − 4 (e) 2.56x + 0.8yarrow_forward
- A steady, three-dimensional velocity field is given byV-›= (0.657 + 1.73x + 0.948y + az) i-› + (2.61 + cx + 1.91y + bz) j-› + (−2.73x − 3.66y − 3.64z)k-› Calculate constants a, b, and c such that the flow field is irrotational.arrow_forwardConsider the steady, two-dimensional velocity field of : V-›= (u, ? ) = (0.5 + 0.8 x) i-›+ (1.5 − 0.8 y) j-› where lengths are in units of m, time in s, and velocities in m/s. There is a stagnation point at (−0.625, 1.875) as shown in Fig. Streamlines of the flow are also plotted in Fig. Calculate the various kinematic properties, namely, the rate of translation, rate of rotation, linear strain rate, shear strain rate, and volumetric strain rate. Verify that this flow is incompressible.arrow_forwardHomework What is the third velocity component such that continuity equation is satisfied if two components are u = 1. 2y2, w = 2хyz ? 2. Consider the following steady, two-dimensional, incompressible velocity field V = (Ax? + B)i + (-Ay + Cx²)j where A, B, and C are constants. Calculate the pressure as a function of x and y.arrow_forward
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