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222 Chapter 5 ■ Finite Control Volume Analysis Section (1) Fixed control volume 30° W 2 T shaft V 1 Section (2) ω D 2 = 2r 2 = 12 in. D 1 = 2r 1 = 10 in. h = 1 in. ω T shaft (a) F I G U R E E5.19 Fixed control volume W 2 W r2 V r2 U 2 V 2 30° V θ2 (b) Then m # The rotor exit blade speed, U 2 , is 16 in.211725 rpm212 rad/rev2 U 2 r 2 112 in./ft2160 s/min2 90.3 ft/s To determine the fluid tangential speed at the fan rotor exit, V 2 , we use Eq. 5.43 to get The vector addition of Eq. 4 is shown in the form of a “velocity triangle” in Fig. E5.19b. From Fig. E5.19b, we can see that To solve Eq. 5 for V 2 we need a value of W 2 , in addition to the value of U 2 already determined (Eq. 3). To get W 2 , we recognize that where V r2 is the radial component of either W 2 or V 2 . Also, using Eq. 5.6, we obtain or since 10.0766 lbm ft 3 21230 ft 3 min2 160 smin2 V 2 W 2 U 2 V 2 U 2 W 2 cos 30° W 2 sin 30° V r 2 m # A 2 V r 2 A 2 2 r 2 h 0.294 lbms (3) (4) (5) (6) (7) (8) where h is the blade height, Eqs. 7 and 8 combine to form m # 2r 2 hV r 2 Taking Eqs. 6 and 9 together we get m # W 2 r2pr 2 h sin 30° rQ r2pr 2 h sin 30° Q 2pr 2 h sin 30° Substituting known values into Eq. 10, we obtain By using this value of W 2 in Eq. 5 we get V 2 U 2 W 2 cos 30° 90.3 ft/s 129.3 ft/s210.8662 64.9 ft/s Equation 1 can now be used to obtain with BG units. With EE units W 2 1230 ft3 min2112 in.ft2112 in.ft2 160 smin22p16 in.211 in.2 sin 30° 29.3 fts 10.294 lbm/s2190.3 ft/s2164.9 ft/s2 W # shaft 332.174 1lbm ft21lbs 2 243550 1ft lb2/1hp s24 (9) (10) 10.00912 slug/s2190.3 ft/s2164.9 ft/s2 W # m # shaft U 2 V 2 31 1slug ft/s 2 2/lb43550 1ft lb2/1hp s24

5.3 First Law of Thermodynamics—The Energy Equation 223 In either case W # shaft 0.097 hp (Ans) COMMENT Note that the “” was used with the U 2 V 2 product because U 2 and V 2 are in the same direction. This result, 0.097 hp, is the power that needs to be delivered through the fan shaft for the given conditions. Ideally, all of this power would go into the flowing air. However, because of fluid friction, only some of this power will produce useful effects (e.g., movement and pressure rise) on the air. How much useful effect depends on the efficiency of the energy transfer between the fan blades and the fluid. 5.3 First Law of Thermodynamics—The Energy Equation The first law of thermodynamics is a statement of conservation of energy. 5.3.1 Derivation of the Energy Equation The first law of thermodynamics for a system is, in words time rate of net time rate of net time rate of increase of the energy addition by energy addition by total stored energy heat transfer into work transfer into of the system the system the system In symbolic form, this statement is D Dt er dVa a Q # in a Q # a a W # in a W # outb sys outbsys sys or D Dt sys er dV1Q # net in W # net2 sys in (5.55) Some of these variables deserve a brief explanation before proceeding further. The total stored energy per unit mass for each particle in the system, e, is related to the internal energy per unit mass, ǔ, the kinetic energy per unit mass, V 2 2, and the potential energy per unit mass, gz, by the equation e ǔ V 2 (5.56) 2 gz The net rate of heat transfer into the system is denoted with and the net rate of work transfer into the system is labeled W # Q # net in, net in. Heat transfer and work transfer are considered “” going into the system and “” coming out. Equation 5.55 is valid for inertial and noninertial reference systems. We proceed to develop the control volume statement of the first law of thermodynamics. For the control volume that is coincident with the system at an instant of time (5.57) Furthermore, for the system and the contents of the coincident control volume that is fixed and nondeforming, the Reynolds transport theorem 1Eq. 4.19 with the parameter b set equal to e2 allows us to conclude that or in words, 1Q # net in W # net2 sys 1Q # net in in D Dt sys er dV 0 0t cv er dV cs erV nˆ dA the time rate the time rate of increase of the total stored of increase of the total energy of the contents stored energy of the control volume of the system W # net2 coincident in control volume the net rate of flow of the total stored energy out of the control volume through the control surface (5.58)

222 Chapter 5 ■ Finite Control Volume Analysis<br />

Section (1)<br />

Fixed control volume<br />

30°<br />

W 2<br />

T shaft<br />

V 1<br />

Section (2)<br />

ω<br />

D 2 = 2r 2 = 12 in.<br />

D 1 = 2r 1 = 10 in.<br />

h =<br />

1 in.<br />

ω<br />

T shaft<br />

(a)<br />

F I G U R E E5.19<br />

Fixed<br />

control volume<br />

W 2<br />

W r2 V r2<br />

U 2<br />

V 2<br />

30° V θ2<br />

(b)<br />

Then<br />

m #<br />

The rotor exit blade speed, U 2 , is<br />

16 in.211725 rpm212 rad/rev2<br />

U 2 r 2 <br />

112 in./ft2160 s/min2<br />

90.3 ft/s<br />

To determine the <strong>fluid</strong> tangential speed at the fan rotor exit, V 2 ,<br />

we use Eq. 5.43 to get<br />

The vector addition of Eq. 4 is shown in the form of a “velocity<br />

triangle” in Fig. E5.19b. From Fig. E5.19b, we can see that<br />

To solve Eq. 5 for V 2 we need a value of W 2 , in addition to the<br />

value of U 2 already determined (Eq. 3). To get W 2 , we recognize<br />

that<br />

where V r2 is the radial component of either W 2 or V 2 . Also, using<br />

Eq. 5.6, we obtain<br />

or since<br />

10.0766 lbm ft 3 21230 ft 3 min2<br />

160 smin2<br />

V 2 W 2 U 2<br />

V 2 U 2 W 2 cos 30°<br />

W 2 sin 30° V r 2<br />

m # A 2 V r 2<br />

A 2 2 r 2 h<br />

0.294 lbms<br />

(3)<br />

(4)<br />

(5)<br />

(6)<br />

(7)<br />

(8)<br />

where h is the blade height, Eqs. 7 and 8 combine to form<br />

m # 2r 2 hV r 2<br />

Taking Eqs. 6 and 9 together we get<br />

m #<br />

W 2 <br />

r2pr 2 h sin 30° rQ<br />

r2pr 2 h sin 30°<br />

Q<br />

<br />

2pr 2 h sin 30°<br />

Substituting known values into Eq. 10, we obtain<br />

By using this value of W 2 in Eq. 5 we get<br />

V 2 U 2 W 2 cos 30°<br />

90.3 ft/s 129.3 ft/s210.8662 64.9 ft/s<br />

Equation 1 can now be used to obtain<br />

with BG units.<br />

With EE units<br />

W 2 1230 ft3 min2112 in.ft2112 in.ft2<br />

160 smin22p16 in.211 in.2 sin 30°<br />

29.3 fts<br />

10.294 lbm/s2190.3 ft/s2164.9 ft/s2<br />

W # shaft <br />

332.174 1lbm ft21lbs 2 243550 1ft lb2/1hp s24<br />

(9)<br />

(10)<br />

10.00912 slug/s2190.3 ft/s2164.9 ft/s2<br />

W # m #<br />

shaft U 2 V 2 <br />

31 1slug ft/s 2 2/lb43550 1ft lb2/1hp s24

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