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fluid_mechanics

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Problems 251<br />

5.47 A converging elbow (see Fig. P5.47) turns water through an<br />

angle of 135° in a vertical plane. The flow cross section diameter is<br />

400 mm at the elbow inlet, section (1), and 200 mm at the elbow outlet,<br />

section (2). The elbow flow passage volume is 0.2 m 3 between<br />

sections (1) and (2). The water volume flowrate is 0.4 m 3 s and the<br />

elbow inlet and outlet pressures are 150 kPa and 90 kPa. The elbow<br />

mass is 12 kg. Calculate the horizontal (x direction) and vertical<br />

(z direction) anchoring forces required to hold the elbow in place.<br />

place. Estimate the nozzle flowrate in ft 3 s. The magnitude of the<br />

velocity of the air remains constant.<br />

5.51 A vertical, circular cross-sectional jet of air strikes a conical deflector<br />

as indicated in Fig. P5.51. A vertical anchoring force of 0.1 N<br />

is required to hold the deflector in place. Determine the mass 1kg2 of<br />

the deflector. The magnitude of velocity of the air remains constant.<br />

F A = 0.1 N<br />

z<br />

Section<br />

(1)<br />

D 1 = 400 mm<br />

135°<br />

x<br />

60°<br />

0.1 m<br />

D 2 =<br />

200 mm<br />

F I G U R E P5.47<br />

Section (2)<br />

5.48 The hydraulic dredge shown in Fig. P5.48 is used to dredge<br />

sand from a river bottom. Estimate the thrust needed from the propeller<br />

to hold the boat stationary. Assume the specific gravity of the<br />

sandwater mixture is SG 1.2.<br />

V = 30 m/s<br />

F I G U R E P5.51<br />

5.52 Water flows from a large tank into a dish as shown in Fig.<br />

P5.52. (a) If at the instant shown the tank and the water in it<br />

weigh W 1 lb, what is the tension, T 1 , in the cable supporting the<br />

tank? (b) If at the instant shown the dish and the water in it weigh<br />

W 2 lb, what is the force, F 2 , needed to support the dish?<br />

T 1<br />

30 ft/s<br />

2-ft diameter<br />

30°<br />

10 ft<br />

Tank<br />

9 ft 7 ft Prop<br />

F I G U R E P5.48<br />

0.1-ft diameter<br />

12 ft<br />

5.49 A static thrust stand is to be designed for testing a specific jet<br />

engine. Knowing the following conditions for a typical test,<br />

intake air velocity 700 fts<br />

exhaust gas velocity 1640 fts<br />

intake cross section area 10 ft 2<br />

intake static pressure 11.4 psia<br />

intake static temperature 480 °R<br />

exhaust gas pressure 0 psi<br />

estimate a nominal thrust to design for.<br />

5.50 A horizontal, circular cross-sectional jet of air having a diameter<br />

of 6 in. strikes a conical deflector as shown in Fig. P5.50.<br />

A horizontal anchoring force of 5 lb is required to hold the cone in<br />

2 ft<br />

Dish<br />

F 2<br />

F I G U R E P5.52<br />

5.53 Two water jets of equal size and speed strike each other as<br />

shown in Fig. P5.53. Determine the speed, V, and direction, u, of<br />

the resulting combined jet. Gravity is negligible.<br />

V<br />

θ<br />

V 2 = 10 ft /s<br />

0.1 ft<br />

60° F A = 5 lb<br />

6 in.<br />

90°<br />

0.1 ft<br />

V 1 =10 ft /s<br />

F I G U R E P5.50<br />

F I G U R E P5.53

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