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90 Sample Chapter

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 
  can write:
dP
=
dz
=
or
Now to find pressure at any point a depth of of the fluid as shown in the figure.
Pressure variation with depth
=
Since
h
o
= constant for incompressible fluid
=
h
o
= P = = pressure head
g
The pressure exerted by a fluid is dependent on the vertical head of the fluid and its specific
weight.
or
The density of incompressible fluid does not remain constant i.e. constant. Now as per
perfect gas equation:
= m
m
but
= density =
=
V
V
Now as per hydrostatic law, the pressure gradient is:
Area = a
Area = a
Area = a
Area = a
dP
dz
P
RT
g
dP
dz
R
P
T
P
RT
        ­ €‚ƒ ƒ „„ m
 €‚ƒ  ƒ „„ ƒ ƒ †‡ ˆ
 ƒ dP = g dz

  
  
 ­
€  

‚
Mercury
  €  ƒ  ƒ „ ƒƒ
 Pressure
High
High pressure line
Gauge pressure
Atm
Low
0
Atmospheric pressure line
Atmospheric pressure
Absolute pressure
Vacuum gauge pressure
Low pressure line
Absolute pressure
Absolute zero vacuum (zero pressure) line
Different Pressures
12. Besides manometers, what are the other types of pressure measuring instruments?
 


­
    13. What are the characteristics of mechanical gauges? Describe Bourdon tube gauge.
    € €    ‚  ƒ ‚   „ 
 ‚            The manometers work on the relationship between the pressure and the column of the fluid
balanced by it. The simplest form of manometers is the pressure tube or piezometer as
shown in the figure. The pressure tube consists of a single vertical tube open at the top
connected to the vessel or pipe containing the fluid under pressure. Due to pressure of the
fluid above the atmospheric pressure, the fluid rises in the tube to a height depending upon
its pressure. If fluid rises meter, then we have gauge pressure of the fluid as:
Vessel with high
pressure fluid (Pabs)
        ­ €
Pabs f
gh f Pabs Patm Pgauge If
l
l ghg
l ghg
Pgauge l ghg
f
l ghg
f
Patm
gh f
f
gh f
Pabs h f
fg
hv
Patm Pabs h f
Pvacuum h f
If
l
lg
fg
fg
Patm
hv
hv
lg
lg
f
Pvacuum hv
lg

       a
dh
 small 1 0
h
alarge 100
 ­ g h dh
h
g(h 0)
gh
h1
h2
1
2
Flow
Flow
Two Piezometer Tubes Method

    
 P h h h
1
2
g
or
P gh
   
h1 g 1 ml
­€    (rml, Sml)
    dP h
Hg g h g
h g
Hg
1 h g SHg 1
  g hS 1 k
P h g
Hg
1 k g
Hg
­ €  ­ € 
a h 0
A 2
P1 f
P2 g h1 dh 1
gh 2
P1 P2
1 2
g
z
g h2 h dh
2
g h2 h dh 2
f
g h1 dh
 A
O2
H2
B
C
   

    

   
 ­ €
 
 ‚
 
    h1 Hg
g
760 13.6 10 3 9.81
1000
h2 Hg
g
660 13.6 10 3 9.81
1000
1014. 88.06 10
12
13.34 10
12
1112 m

3
3
­€ ­­
  ­   ­ Pr = 230 kpa
Air
h
Water
Hg
2
1 120 cm
P1 = 140 kpa
    ­ €  P1 120
. Hg
gh
3
g Pair
. 13.6 10 9.81 h 103 9.81 230
400 120
103
103
160 9.81 h 230
h 10 102
. m
9.8
Let = absolute pressure of the water in the pipeline during equilibrium –
Pressure in the left limb from datum = Pressure in the right limb from datum
P1 100 1000
w
g 100 100 1000
Hg
g Patm
3
. 103 g 9.81
01
P1 Patm 0.2 13.6 10 9.81 1000
1000
Pgauge 26.68 0.981
Pgauge 25.7 kpa
27. The figure shows a conical vessel having a U tube manometer attached to its outlet
at . When the vessel is empty the reading of the manometer is given in the figure.
Find the reading of manometer when the vessel has been completely filled with water.
A
When the vessel is empty, the pressure in both limbs is same from datum line – Pressure left limb = Pressure in right limb
0.24 12
. 103 g h 0.8 103 g
0.288 + 0.8
0.2
=
=
=
=
=
(0.24 h)1 103
0.24 + 0.078
0.39 m
390 mm
 

h1
Equating pressure on left and right limb from datum line – Pa (2 h h1 )
1
g = Pb h
2g
h1
1g
0.5 105 (2 h) 103 9.8 = 0.2 105 h 13.6 103 9.8
0.3 102 (2 h )9.81 = 13.6 9.81 h
49.62 0.401 m
126.6
   
 
PA 1 10 3 9.81 sin 30 h1 h 13.6 10 3 h 9.81 1 10 3 h1 h 9.81 PB
2
2
3
PA PB 10 9.81(13.6 .14 1 0.14)
9.83 10 3 (0.764)
 
   PA 0.24 0.8 10 3 g
P1 0.10 .8 10 3 g
0.12 13.6 10 3 g P1
0.15 13.6 10 3 g
or P1 PA 1.88 10 3 16 10 3
0.10 0.8 10 3 g PB
PA 14.12 10 3
or P1 PB 20.01 10 3
   
 32. A multi tube manometer is employed to determine the pressure in a pipeline. The
levels inside the tubes are as shown in the figure. What would be the length of single
mercury U-tube to record this pressure?
­ 3
PA 0.5 13.6 10 g P1
3
PA 66.7 10 P1
P1 .5 1 10 3 g
.5 13.6 10 3 g P2
P1 61.8 10 3 P2
66.7 10 3 Patm P2 0.5 1 10 3 g
Patm .5 13.6 10 3 g
P2 Patm 61.8 10 3
61.8 10 3 Patm 123.6 10 3
61.8 10 3
200.3 10 3 Patm
P1 Patm 123.6 10 3
PA Patm Pgauge 200.3 kPa
In case we have ample U tube manometer, then,
– = 200.3 10 = 13.6 10 9.81
=
200.3
= 1.5 m
13.6 9.81
PA h1 2 g P1
from eqn (1)
PB 2 hg 1hg P1
P1 PB hg ( 2 1 ) eqn (1)
PA h1 2 g PB hg( 2 1 )
PA PB ( 2 1 )gh 2 h1 g
PA h1
2 g h2 1
PA PC (h1
2g
g PC
h2
1g)
    
­€­ €
PB h1 1 10 3 g h .875 10 3 g P1
PA (h1 h) 1 10 3 g P1
PA (h1 h) 1 103 g PB h .875 103 g h1 1 103 g

0.12 10 3 9.81 0.125
  PA h 115
. 10 3 g
P1 .20 0.92 10 3 g
P1 (.50 h) 115
. 10 3 g PB
PA h 115
. 10 3 g 0.2 0.92 10 3 g
. 10 3 g
PB (.5 h) 115
PA PB 0.2 0.92 10 3 g 0.5 115
. 10 3 g
1.8 10 3 5.64 10 3
384
. 103 kPa
3
3.843 10
1 10 9.81
391 mm of water
 
     ­ PM P1 Y 0.8 10 3 g
P1 0.75 0.8 10 3 9.81
P1 Patm Z 13.6 10 3 g
P1 Patm 0.25 13.6 10 3 9.81
PM 0.75 0.8 103 9.81
Patm 0.25 13.6 103 9.81
0.25 13.6 103 9.81 0.75 0.85 103 9.81
(33.35 6.25) 10 3
39.6 10 3 Pa

 € PA PB 1 a r2 r1 gh A
     (0.06) 2
0.0028
4
15 1000 5.36 106 N/m2
0.0028
4

 .000314 5.36 10 6
1684 N
(0.02) 2
F 30 1684 30
400
400
C
70 cm
 


  ­ ­
  ‚ ƒ €­ ­
7.85 kN2
m
ƒ €­
­ƒ „   „
‚ 3
0.9 10 39.81 2.0 6.867
10
17.658 6.87
24.528 kN2
m
l1
l2
Pair 1 g P1
0.4 0.8 103 9.81 P1
103
314
. P1
Patm 3
Hg g
P1
3
P1 Patm 0.9 13.6 310 9.81
10
Patm 120.07
     ­ €‚
  €‚
      
­ € ‚
   h a l 1 0.8 0.04 m
A
20
h l sin 0.8 1
2
ƒ ­
dy dA g
y y dy
dp 1000 g 1 100 1000 y y y 200 3 10 9810 80 6400 512 10 200
3 10 1 y
y
500
1000
2
2
2
1
2
80
3
6
0
3
6
     ρ s = 1030
1500 mm
ρ =?
d
dP
K
dP
d
d dP
K
    (1030) 9.81 1500
2.4 109
. 106 9.81 15
. 103
106
2.4 109
6.5 kg/m3
 ­ € ‚€
‚€ ƒ
     
­ €
‚ ƒ„   ­­€‚
­‚    Water
Oil
Horizontal
plane
Pipes
Horizontal
plane
Mercury
  ­  ­­ ƒ   ­  ­­ 
  ­  ­­ 
 ­  ­­    „ †
† ‡
ˆ ˆ ƒ „
‰ ‚ ƒ „      ­ ­ ‡   ­    ­   ƒ € H h
 S+
h1
h
Dh
 
  
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 ­­€

       
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