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Consider steady flow of water through an axisymmetric garden hose nozzle (Fig. 9-28). Suppose the axial component of velocity increases linearly from
FIGURE P9-28
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Fluid Mechanics: Fundamentals and Applications
- Problem 1 Given a steady flow, where the velocity is described by: u = 3 cos(x) + 2ry v = 3 sin(y) + 2?y !! !! a) Find the stream function if it exists. b) Find the potential function if it exists. c) For a square with opposite diagonal corners at (0,0) and (47, 27), evaluate the circu- lation I = - f V.ds where c is a closed path around the square. d) Calculate the substantial derivative of velocity at the center of the same box.arrow_forwardflow in a pipe questions e-garrow_forwardfluid mechanicsarrow_forward
- Kindly give a detail and corrrect solution with proper explanation. I will give like else dislikearrow_forwardConsider a steady, two-dimensional, incompressible fl owof a newtonian fl uid in which the velocity fi eld isknown: u = - 2 xy , υ = y 2 - x 2 , w = 0. ( a ) Does thisfl ow satisfy conservation of mass? ( b ) Find the pressurefi eld, p ( x , y ) if the pressure at the point ( x = 0, y = 0) isequal to p a .arrow_forwardIn the fig-Shown, the Flow rate Pipe (A) is equal ( QA= 25 Lit15), he diameter is equal ( DA = 75mm, Do 60mm, De = Dc =30 mm). and the velocity in Pipe (D) is equal ( 40=5m/s). the relation between flow rate in Pipe (B) and pipe (c) in %3D %3D PB =3 Qc. Find the Ualue of .. 2- UA, UB, Uc: Pe =30 mm water Pc = 30 mm imput QA = 25 2it/sec = 75 mm Po = 6omm input = A outPut = B, C, D accumu lation = o.arrow_forward
- (Fluid) 1arrow_forwardi need the answer quicklyarrow_forwardb Water flows around the vertical two-dimensional bend with circular streamlines and constant velocity as shown in the figure below. If the pressure is 62 kPa at point (1), determine the pressures at points (a) (2) and (b) (3). Assume that the velocity profile is uniform as indicated. = Esc Type here to search L 1 A 30 @ 2 W S 4x F2 # 3 E 4₁ D O $ 4 R F F4 % 5 2m 99+ FS T G A 6 4 m 1 m Y H (3) (2) (1) * F7 & 7 V = 10 m/s U PrtScn FB 8 Home 9 K 9 End F10 ) 0 L 36°F Clear PgUp F11 P PgDn 40 + (1) 7:00 PM 11/21/2022 Del Backsparrow_forward
- Fluid Mechanics Question An incompressible fluid flows in the converged nozzle provided in the figure. nozzle area -> A=Ao*(1-b*x) entry speed -> V=Vo*(0.5+0.5*cos(w*t)) Vo:20m/s Ao=1.5 m2 L=13m b=0.2/22 W=0.16rad/s Find the acceleration in the nozzle center as a function of time * (to multiplication) / (to divide)arrow_forwardConsider steady, incompressible, two-dimensional flow through a converging duct (Figure below). Uo A simple approximate velocity field for this flow of the Converging duct flow is modeled by the steady, two- dimensional velocity field given by: V = (u, v) = (U, + bx)i – byj The pressure field is given by: P = P, – 2U,bx + b*(x² + y²) Where Po is the pressure at x = 0. Generate an expression for the rate of change of pressure following a fluid particle?arrow_forwardI need the answer as soon as possiblearrow_forward
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