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tatuchka [14]
3 years ago
7

Steam enters a nozzle at 400°C and 800 kPa with a velocity of 10 m/s and leaves at 375°C and 400 kPa while losing heat at a rate

of 27 kW. For an inlet area of 800 cm^2, determine the velocity and the volume flow rate of the steam at the nozzle exit. Use steam tables.
Engineering
1 answer:
GenaCL600 [577]3 years ago
5 0

Answer:

Using the equation of continuity:

A

1

v

1

=

A

2

v

2

0.08

(

10

)

=

A

2

(

225

)

A

2

=

3.55

×

10

−

3

m

2

Q

2

=

A

2

v

2

Q

2

=

3.55

×

10

−

3

×

225

Q

2

=

0.798

m

3

/

s

Explanation:

Steady Flow Energy Equation:

The steady flow energy equation is a representation of the first law of thermodynamics. It is the conservation of energy law for an open system. A nozzle is an open system in the context of thermodynamics. It is used to produce a high velocity by reducing its pressure.

The steady flow energy equation can be given by the following formula:

h

1

+

1

2

v

2

1

+

g

z

1

+

q

=

h

2

+

1

2

v

2

2

+

g

z

2

+

w

where 'h' is enthalpy, 'v' is velocity, 'z' is height, 'q' is the heat and 'w' is work.

h

=

C

p

d

T

Answer and Explanation:

Given:

initial temp,

T

1

=

400

0

C

initial Pressure,

p

1

=

800

k

P

a

Initial Velocity,

v

1

=

10

m

/

s

Final temp,

T

2

=

300

0

C

Final Pressure,

p

2

=

200

k

P

a

Rate of heat loss, Q = 25 KW

Inlet Area,

A

1

=

800

c

m

2

As per the steady flow energy equation:

h

1

+

1

2

v

2

1

+

g

z

1

+

q

=

h

2

+

1

2

v

2

2

+

g

z

2

+

w

Since, there is external work, w= 0. Also, consider there is a negligible change in KE.

h

1

+

1

2

v

2

1

+

q

=

h

2

+

1

2

v

2

2

h

1

−

h

2

+

1

2

v

2

1

+

q

=

1

2

v

2

2

C

p

(

T

1

−

T

2

)

+

1

2

(

10

)

2

+

25000

=

1

2

v

2

2

2

(

400

−

300

)

+

50

+

25000

=

1

2

v

2

2

2

(

400

−

300

)

+

50

+

25000

=

1

2

v

2

2

25250

=

1

2

v

2

2

v

2

≈

225

which is the answer.

Using the equation of continuity:

A

1

v

1

=

A

2

v

2

0.08

(

10

)

=

A

2

(

225

)

A

2

=

3.55

×

10

−

3

m

2

Now, volume flow rate,

Q

2

=

A

2

v

2

Q

2

=

3.55

×

10

−

3

×

225

Q

2

=

0.798

m

3

/

s

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Greeley [361]

Answer:

D) 1.04 Btu/s from the liquid to the surroundings.

Explanation:

Given that:

flow rate (m) = 2 lb/s

liquid specific enthalpy at the inlet (h_{1}=40.09 Btu/lb)

liquid specific enthalpy at the exit (h_{2}=40.94 Btu/lb)

initial elevation (z_1=0ft)

final elevation (z_2=100ft)

acceleration due to gravity (g) = 32.174 ft/s²

W_{cv} = 3 Btu/s

The energy balance equation is given as:

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Since  kinetic energy effects are negligible, the equation becomes:

Q_{cv}-W{cv}+m[(h_1-h_2)+g(z_1-z_2)]=0

Substituting values:

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A hollow, spherical shell with mass 2.00kg rolls without slipping down a slope angled at 38.0?.
mezya [45]

Answer:

\mu = 0.31

Explanation:

Given data:

mass = 2.00 kg

slope angle = 38.0

From figure

balancing force

mgsin\theta - f = ma   .....1

Balancing torque

F_R = \frac{2}{3} mR^2 \alpha ......2

for pure rolling

\alpha  = \frac{a}{R}

F = \frac{2}{3} ma

from 1 and 2nd equation

mgsin\theta - \frac{2}{3}ma =  ma

mgsin\theta = \frac{5}{3} ma

a = \frac{3}{5} g sin\theta

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F =\mu N

   = \frac{2}{3} ma

   = \frac{2}{3} 2\times 3.62 = 4.83 N

N =normal force =  mgsin\theta = 2 \times 9.8 sin 38 = 15.44 N

\mu \times 15.44 = 4.83

solving for  coefficent of friction we get

\mu = 0.31

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