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5.2 Newton’s Second Law—The Linear Momentum and Moment-of-Momentum Equations 207<br />

F l u i d s i n t h e N e w s<br />

Motorized surfboard When Bob Montgomery, a former professional<br />

surfer, started to design his motorized surfboard<br />

(called a jet board), he discovered that there were many engineering<br />

challenges to the design. The idea is to provide surfing<br />

to anyone, no matter where they live, near or far from the ocean.<br />

The rider stands on the device like a surfboard and steers it like<br />

a surfboard by shifting his/her body weight. A new, sleek, compact<br />

45-horsepower engine and pump was designed to fit within<br />

the surfboard hull. Thrust is produced in response to the change<br />

in linear momentum of the water stream as it enters through the<br />

inlet passage and exits through an appropriately designed nozzle.<br />

Some of the <strong>fluid</strong> dynamic problems associated with designing<br />

the craft included one-way valves so that water does not<br />

get into the engine (at both the intake or exhaust ports), buoyancy,<br />

hydrodynamic lift, drag, thrust, and hull stability. (See<br />

Problem 5.68.)<br />

To further demonstrate the use of the linear momentum equation 1Eq. 5.222, we consider<br />

another one-dimensional flow example before moving on to other facets of this important<br />

equation.<br />

E XAMPLE 5.12<br />

Linear Momentum—Pressure and Change in Flow Direction<br />

FIND Calculate the horizontal 1x and y2 components of the anchoring<br />

2 stant at a value of through the bend. The magnitude of the<br />

GIVEN Water flows through a horizontal, 180° pipe bend as<br />

on the <strong>fluid</strong> and the pipe bend are resolved and combined into the<br />

two resultant components, F Ax and F Ay . These two forces act on vrV nˆ dA F Ay p 1 A 1 p 2 A 2<br />

cs<br />

(2)<br />

illustrated in Fig. E5.12a. The flow cross-sectional area is con-<br />

force required to hold the bend in place.<br />

2 0.1 ft<br />

flow velocity everywhere in the bend is axial and 50 fts. The<br />

absolute pressures at the entrance and exit of the bend are 30 psia<br />

and 24 psia, respectively.<br />

SOLUTION<br />

Since we want to evaluate components of the anchoring force to At sections 112 and 122, the flow is in the y direction and therefore<br />

hold the pipe bend in place, an appropriate control volume 1see u 0 at both cross sections. There is no x direction momentum<br />

dashed line in Fig. E5.12a2 contains the bend and the water in the flow into or out of the control volume and we conclude from Eq. 1<br />

bend at an instant. The horizontal forces acting on the contents of that<br />

this control volume are identified in Fig. E5.12b. Note that the<br />

weight of the water is vertical 1in the negative z direction2 and<br />

F Ax 0<br />

(Ans)<br />

does not contribute to the x and y components of the anchoring For the y direction, we get from Eq. 5.22<br />

force. All of the horizontal normal and tangential forces exerted<br />

the control volume contents, and thus for the x direction, Eq. 5.22<br />

leads to<br />

For one-dimensional flow, the surface integral in Eq. 2 is easy to<br />

evaluate and Eq. 2 becomes<br />

urV nˆ dA F Ax<br />

cs<br />

(1) 1v 1 21m # 12 1v 2 21m # 22 F Ay p 1 A 1 p 2 A 2 (3)<br />

V =<br />

50 ft/s<br />

V = 50 ft/s<br />

x<br />

Section (1) A = 0.1 ft 2<br />

z<br />

Section (2)<br />

y<br />

(a)<br />

F I G U R E E5.12<br />

Control<br />

volume<br />

180° pipe bend<br />

x<br />

z<br />

w<br />

u v y<br />

p 1 A 1<br />

v 1<br />

Pipe bend<br />

and water<br />

F Az<br />

F Ay<br />

p 2 A 2<br />

v 2<br />

<br />

Control volume<br />

(b)<br />

F Ax

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