Converging duct flow is modeled by the steady, two-dimensional velocity field of Prob. 4—16. A fluid particle ( A ) is located at x = x A and y at time t = 0 (Fig. P4—54). At some later time i. the fluid particle has moved downstream with the flow to some new location x = x A , y = y A , as shown in the figure. Generate an analytical expression for the -location of the fluid particle at arbitrary time t in terms of its initial y-location and constant b. In other words, develop an expression for. (Hint: We know that v = d y particle following a fluid particle. Substitute the equation for u, separate variables, and integrate.)
Converging duct flow is modeled by the steady, two-dimensional velocity field of Prob. 4—16. A fluid particle ( A ) is located at x = x A and y at time t = 0 (Fig. P4—54). At some later time i. the fluid particle has moved downstream with the flow to some new location x = x A , y = y A , as shown in the figure. Generate an analytical expression for the -location of the fluid particle at arbitrary time t in terms of its initial y-location and constant b. In other words, develop an expression for. (Hint: We know that v = d y particle following a fluid particle. Substitute the equation for u, separate variables, and integrate.)
Converging duct flow is modeled by the steady, two-dimensional velocity field of Prob. 4—16. A fluid particle (A) is located at x = xAand y at time t = 0 (Fig. P4—54). At some later time i. the fluid particle has moved downstream with the flow to some new location
x
=
x
A
,
y
=
y
A
, as shown in the figure. Generate an analytical expression for the -location of the fluid particle at arbitrary time t in terms of its initial y-location and constant b. In other words, develop an expression for. (Hint: We know that
v
=
d
y
particle
following a fluid particle. Substitute the equation for u, separate variables, and integrate.)
Kindly solve Question 2 complete only this is complete Question 2 nothing more information is provided for this question
For a certain two-dimensional incompressible flow, velocity field is given
by 2xy î - y?j. The streamlines for this flow are given by the family of
curves
Dentrance
x=0
uentrance
FIGURE P4-21
u(x)
lexit
x = L
Dexit
4-22 For the velocity field of Prob. 4-21, calculate the
fluid acceleration along the diffuser centerline as a function
of x and the given parameters. For L = 1.56 m, uentrance =
22.6 m/s, and exit = 17.5 m/s, calculate the acceleration at
x = 0 and x = 1.0 m. Answers: 0, -96.4 m/s²
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