Pressure drop calculation - theory
In this calculator well known equations have been used. Here you can find all of them for your review. First of all, pressure drop through the pipe due to friction and local losses can be calculated as follows:
where is:
Dp - pressure drop rho - fluid density view table Q - volumetric flow rate D - pipe diameter lambda - friction coefficient L - pipe length sum ksi - the sum of minor losses coefficient
To calculate mass flow rate following equation has been used: where is:
G - mass flow rate
For pressure drop calculation because of friction, viscosity of fluid has to be known. Relation between dynamic and kinematic viscosity is as follows: where is:
mi - dynamic viscosity view table ni - kinematic viscosity view table
Velocity of flowing fluid is calculated based on the continuity equation:
where the cross section of round pipe is:
To find out if the flow is laminar or turbulent, Reynolds number must be calculated:
Friction coefficient for laminar flow is:
for flow in hydraulically smooth pipe (Blasius equation):
for turbulent flow with Re<100 000 (Prandtl equation):
for turbulent flow with Re>100 000 (Karman equation):
The boundary layer thickness (delta) can be calculated based on the Prandtl equation as:
and when the boundary layer thickness is bigger than pipe roughness and if the flow is turbulent, than it can be considered as flow in hydraulically smooth pipe and Blasius equation is used.
Pipe diameter calculation - theory
Pipe diameter can be calculated when volumetric flow rate and velocity is known as:
where is:
D - pipe diameter Q - volumetric flow rate V - velocity If mass flow rate is known than diameter can be calculated as:
where is: G - mass flow rate rho - fluid density view table If the flowing fluid is gas than the density can be calculated if pressure, temperature and gas constant is known as:
where is:
p - pressure
T - temperature R - gas constant view table It is important to say that the flow rate is depending on the pressure difference between two points. This calculator is for the calculation if you already know the flow rate. If the flow rate is to be calculated also, than you should use pressure drop calculator.
Control valve sizing calculation
It is well known that for the completely turbulent flow relationship between fluid flow rate and pressure drop follows the power low. Flow coefficient is the proportional constant between pressure drop and flow rate and it is determined experimentally by valve manufactures. It is expressed as the flow rate of water in gpm u.s. (m3/h) for a pressure drop of 1 psi (1 bar) across a flow passage. note: (flow coefficient: Cv-imperial, Kv-metric) For correct control valve sizing it is important to calculate flow coefficient using this calculator. When flow coefficient is calculated for required flow rate and known pressure drop, selection of proper control valve can be done by selecting control valve with first bigger flow coefficient. Also using this calculator you can calculate maximum flow rate through control valve for given pressure drop and known flow coefficient or valve size. This version of calculator can be used for turbulent flow of water or other incompressible fluid, as viscosity and expansion effect is not included. It means that for steam and gas control valve you will need to use other calculation methods. Also, possible flashing and cavitation may reduce the control valve capacity, as it is not treated in this version calculator. Read about used theory for control valve sizing calculation
Control valve sizing calculation - theory
Control valve sizing is based on the calculation of flow coefficient for given pressure drop and fluid flow rate. Main equation that gives relation between flow rate and pressure drop is:
for imperial units, and:
for metric units, where is:
Cv - flow coefficient in imperial units Kv - flow coefficient in metric units Dp - pressure drop through control valve Q - fluid flow rate
G - specific gravity view table ro - relative density view table
Flow coefficient is defined as the proportional constant between pressure drop and flow rate and it is determined experimentally by valve manufactures. It is expressed as the flow rate of water in gpm u.s. (m3/h) for a pressure drop of 1 psi (1 bar) across a flow passage. note: (flow coefficient: Cv-imperial, Kv-metric) Relation between volumetric and mass flow rate is calculated using well known equation: Also, velocity or pipe diameter can be calculated using following equations:
Venturi tube flow calculation
Based on the energy conservation low, Venturi tube is one of the easiest to use, not expensive and very accurate instrument for flow rate measuring of water, air, gas or any other fluid in pipe systems. Measure pressure drop from the inlet to the throat and calculate flow rate using this free calculator. Flow through Venturi tube calculator can be used for both liquids and gases. Fluid is considered as incompressible, so density (rho) and temperature (T) are constant through tube. Also, gas is considered as ideal. Read about used theory in flow through Venturi tube calculation
Venturi tube flow calculation - theory
Calculation of flow through the Venturi tube is for incompressible flow, based on the Bernoulli principle:
where is: p - pressure rho - density view table V - velocity g - gravitational constant (9.81 m/s2) z - geodetic height Assumption that pressure lost is negligible:
and:
and if velocities substituted with flow rate:
where is: Q - volumetric flow rate D - diameter Pressure drop through the Venturi tube because of velocity increase can be calculated as follows:
or:
Expressing flow rate from the previous equation leads to:
Substituting:
flow rate can be determined as:
where C is coefficient of discharge. The above equation is main one used for flow calculation in calculator. Other values are calculated using following equations: mass flow:
velocities:
If the calculator is used for gas flow, then gas is considered as incompressible and ideal. Equation for ideal gas:
can be used for calculation of temperature T:
as well as density rho:
where R is gas constant (R=287 J/kgK for air) Coefficient of discharge C As fluid exits a reservoir through a small hole and enters another one, or flows out to the open air, stream lines tend to contract itself, mostly because of inertia. Coefficient of discharge C is used to include this effect. For the Venturi tubes with diameters in range of D = (200 - 1200 mm), D2/D1 = (0.4 - 0.7) and ReD = (2 ·105 - 2 ·106) the coefficient of discharge is C = 0.985. In this calculator for coefficient off discharge C following equation has been used:
where a, b, and c depend on the type of Venturi tube. For welded tube, these coefficients are: a=0.70304970 b=0.00490015 c=-0.00024547 For casted tube are: a=0.60892370 b=0.00659844 c=-0.00033123 And for machined are: a=0.49670179 b=0.00873339 c=-0.00044367 Reynolds number on inlet ReD is calculated using well known equation:
Orifice plate flow calculation
Orifice plate is used for flow rate measuring in pipe systems. With orifice plate, pressure drop is created. Based on the value of pressure drop, flow rate can be calculated. This instrument is very practical for large tube diameters and for dirty fluid when turbines are not applicable. Measure pressure drop from position 1 to position 2 and calculate flow rate and more with this easy to use calculator Orifice plate calculator can be used for both liquids and gases. Fluid is considered as incompressible, so density (rho) and temperature (T) are constant through tube. Also, gas is considered as ideal. Read about used theory for flow through orifice calculation.
Orifice plate flow calculation - theory
Calculation of flow rate using orifice plate calculator is for incompressible flow, based on the Bernoulli principle:
where is: p - pressure rho - density view table V - velocity g - gravitational constant (9.81 m/s2) z - geodetic height Assumption that pressure lost is negligible (pressure drop is obvious and included with coefficient of discharge which is introduced bellow):
and:
and if velocities substituted with flow rate:
where is: Q - volumetric flow rate D - diameter Pressure drop through the orifice because of velocity increase can be calculated as follows:
or:
Expressing flow rate from the previous equation leads to:
Substituting:
flow rate can be determined as:
where is: C - coefficient of discharge e - expansion coefficient Coefficient of discharge can be calculated using following equation (ISO):
where is: beta - diameter relation D2/D1 ReD - Reynolds number which can be calculated as follows:
where is: ni - kinematic viscosity view table mi - dynamic viscosity view table L1 and L2 are functions on tap type and it is: L1=L2=0 for corner taps L1=1 L2=0.47 for D & D/2 taps L1=L2=0.0254/D D[m] for 1" taps Expansion coefficient e can be calculated (for gases only):
where is: kappa - isentropic coefficient; kappa = 1.4 for air and other two atom gas molecules view table Other values are calculated using following equations: mass flow:
velocities:
If flowing fluid is gas, then it is considered as incompressible and ideal. Equation for ideal gas:
can be used for calculation of temperature T:
as well as density rho:
Tables of fluid physical propetries Here you can find the list of available fluid properties tables which can be used in calculators on this site: Dry air This table gives values of some dry air physical properties in relation to temperature and pressure. Gases This table gives values of some physical properties of some gases Flue gases This table is for flue gases. It gives values of some physical properties in relation to the temperature of gases. Water This table gives values of some water physical properties in realtion to temperature. For temperatures higher than 100 OC, it is for water boiling conditions. Steam This table gives values of some saturated steam physical properties in realtion to temperature.
Physical properties of dry air Available tables: dry air gases flue gases water steam This table gives values of some dry air physical properties in relation to temperature and pressure. t [OC]
-50
0
50
100
150
200
300
400
1 bar
1.563
1.275
1.078
0.932 0.8226 0.7356 0.6072 0.517
50 bar
83.794
65.198 53.964 46.25 40.57
36.18
29.8
25.37
100 bar
175.648 131.36 107.07 91.13 79.66
70.92
58.37
49.71
200 bar
340.34
253.7
205.4
174.3 152.2
135.6
111.8
95.41
300 bar
449.3
350.8
288.6
246.7 216.4
193.4
160.3
137.4
Density rho [kg/m3]
Specific heat cp [kJ/kgK]
1 bar
1.007
1.006
1.008
1.012 1.018
1.026
1.046
1.69
50 bar
1.212
1.112
1.085
1.075 1.055
1.049
1.061
1.08
100 bar
1.43
1.216
1.133
1.096 1.078
1.072
1.075
1.09
200 bar
1.623
1.361
1.229
1.161 1.126
1.108
1.099
1.107
300 bar
1.604
1.409
1.282
1.204 1.16
1.135
1.117
1.12
1 bar
14.65
17.2
19.61
21.82 23.92
25.85
29.47
32.76
50 bar
16.7
19.42
20.57
22.59 24.4
26.4
29.9
33.1
100 bar
18.3
20.2
21.7
23.4
25.1
26.9
30.4
33.5
200 bar
22.8
23.6
24.4
25.6
26.8
28.5
31.5
34.7
300 bar
28.7
27.8
27.5
28.1
28.8
30.1
33.1
36.1
Dynamic viscosity mi*106 [Pas]
Physical propetries of gases Available tables: dry air gases flue gases water steam This table gives values of some physical properties of some gases.
GAS
Gas density
Molar weight
Gas constant
Spec. heat at 20OC and 1 bar
rho
M*103
R
Cp
[kg/m3]
[kg/mol]
[J/kg*K]
[J/kg*K] [J/kg*K] [-]
[Pa*s] - 0OC and 1 bar
Cv
Dynamic viscosity
kapa=Cp/Cv mi*106
Acethylene
C2H2
1.171
26.04
319.6
1683
1352
1.25
9.35
Ammonia
NH3
0.771
17.03
488.3
2219
1680
1.37
9.18
Argon
Ar
1.782
39.94
208.5
532
322
1.65
20.9
Nitrogen
N2
1.251
28.02
296.7
1047
746
1.4
17
Nitrogen Oxide
NO
1.34
30.01
277.1
975
696
1.38
17.8
Butane
C4H10
2.673
58.12
143.2
1917
1733
1.108
8.1
i-Butane
C4H10
2.668
58.12
143.2
1632
-
-
7.47
Ethane
C2H6
1.357
30.06
276.7
1729
1445
1.2
8.5
Ethylene
C2H4
1.261
28.05
296.6
1528
1222
1.25
9.85
Ethyl Ether
C4H10O -
74.12
112.2
2302
-
-
286
Ethyl Chloride
C2H5Cl -
64.5
129
1340
-
-
9.4
Helium
He
0.178
4.002
2079
5274
3181
1.66
18.8
Chlor
Cl2
3.217
70.91
117.3
481
355
1.36
12
Hydrogen Chloride
HCl
1.639
36.47
228
812
583
1.4
-
Oxygen
O2
1.429
32
259.9
913
653
1.4
20.3
Krypton
Kr
3.708
83.7
100.3
251
151
1.67
23.2
Xenon
Xe
5.851
131.3
63.84
159
96.3
1.7
21
Methane
CH4
0.717
16.03
518.8
2225
1700
1.31
10.3
Methyl Chloride
CH3Cl
2.308
50.48
164.8
741
582
1.28
9.89
Neon
Ne
0.9002
20.18
411.7
1038
620
1.68
29.7
Ozone
O3
2.22
48
173.4
-
-
1.29
-
Pentane
C5H12
-
72.1
115.2
1717
1575
1.09
8.74
Propane
C3H8
2.02
44.06
188.8
1863
1650
1.13
7.95
Propene
C3H6
1.914
42.05
198.8
1635
1437
1.17
8.35
Sulphur Dioxide
SO2
2.927
64.06
129.8
633
503
1.25
11.7
Sulphur Hydrogen
H2S
1.539
34.09
244.2
1059
804
1.3
11.66
Carbon Dioxide
CO2
1.976
44.01
189
837
653
1.3
13.7
Carbon Monoxide CO
1.25
28.01
297
1047
754
1.4
16.6
Air
1.293
28.95
287
1010
720
1.4
17.3
0.08985
2.016
4125
14266
10130
1.407
8.42
Hydrogen
H2
This table gives values of some physical properties in relation to the temperature of gases. GAS
Nitrogen
Argon
N2
Ar
t [OC]
0
100
200
300
400
500
600
700
cp [kJ/kgK]
1.039
1.042
1.052
1.069
1.091
1.115
1.139
1.161 1.181
mi*106 [Pas]
16.6
20.8
24.6
28
31.1
33.9
36.6
39
41.3
lambda*103 [W/mK] 24.31
31.52
38.5
44.89
50.71
55.82
60.36
64.2
67.45
cp [kJ/kgK]
0.522
0.521
0.521
0.521
0.521
0.52
0.52
0.52
0.52
mi*106 [Pas]
21.2
27.1
32.1
36.7
41
45.22
48.7
21.17
25.59
29.89
33.96
37.91
39.43
1.591
2.026
2.453
2.813
3.127
3.403
3.642
6.84
9.26
11.67
14.03
16.38
18.74
21.09
lambda*103 [W/mK] 13.26
23.5
36.52
51.87
29.78
90.25
113
cp [kJ/kgK]
1.647
2.067
2.49
2.87
3.214
3.519
3.787
mi*106 [Pas]
8.55
11.5
14.1
16.4
19
21.4
23.8
lambda*103 [W/mK] 18
31.7
47.7
65.9
cp [kJ/kgK]
1.406
1.737
2.064
2.394
2.721
3.052
3.382
3.709 4.039
mi*10 [Pas]
9.6
12.7
15.6
18.2
20.6
22.8
24.9
26.8
lambda*103 [W/mK] 16.51 Butane
C4H10 cp [kJ/kgK] mi*106 [Pas]
Ethane
Ethylene
C2H6
C2H4
6
800
4.022 4.216
28.7
Helium
He
Oxygen
O2
Methane
CH4
lambda*103 [W/mK] 16.4
29.54
44.19
59.43
75.71
92.34
108.39 123.3 134.9
cp [kJ/kgK]
5.204
5.204
5.204
5.204
5.204
5.204
5.204
mi*106 [Pas]
18.74
22.96
26.98
30.8
34.33
37.57
40.32
lambda*103 [W/mK] 143
179.1
212.8
244.2
275.6
304.7
332.6
cp [kJ/kgK]
0.915
0.934
0.963
0.995
1.024
1.048
1.069
1.086 1.1
mi*106 [Pas]
19.2
24.4
29
33.1
26.9
40.3
43.5
46.5
49.3
lambda*103 [W/mK] 24.66
32.91
40.7
48.03
55.01
61.52
67.45
72.8
77.69
cp [kJ/kgK]
2.165
2.448
2.807
3.175
3.529
3.856
4.153
4.421 4.659
mi*10 [Pas]
10.4
13.3
16.1
18.5
20.8
22.7
24.6
26.5
lambda*103 [W/mK] 30.24
41.29
51.87
62.34
72.22
81.88
91.3
100.5 109.3
cp [kJ/kgK]
1.549
2.017
2.458
2.834
3.161
3.449
3.697
3.916 4.093
7.5
10.06
12.48
14.75
17.15
19.4
21.8
lambda*10 [W/mK] 15
27.4
41.7
57.9
76
95.8
cp [kJ/kgK]
1.426
1.8
2.16
2.476
2.753
2.991
3.2
3.388 3.54
mi*10 [Pas]
7.84
10.73
13.4
15.92
lambda*103 [W/mK] 14
25.6
38.9
53.7
cp [kJ/kgK]
0.607
0.662
0.712
0.754
0.783
0.808
0.825
0.837 0.85
mi*106 [Pas]
12.1
16.1
20
23.8
27.5
31.3
35
38.6
lambda*103 [W/mK] 8.37
12.33
16.63
21.17
25.82
30.7
35.82
41.05 46.29
cp [kJ/kgK]
0.815
0.914
0.993
1.057
1.11
1.155
1.192
1.223 1.249
mi*106 [Pas]
13.8
18.4
22.6
26.4
29.9
33.2
36.2
38.1
lambda*103 [W/mK] 14.65
22.79
30.94
39.08
47.22
54.89
62.1
68.85 75.13
cp [kJ/kgK]
1.104
1.045
1.058
1.08
1.106
1.132
1.157
1.179 1.999
mi*106 [Pas]
16.6
20.9
24.6
27.8
39
33.8
36.3
38.7
30.12
36.52
42.57
48.5
54.08
59.66
65.01 70.13
6
Propane
C3H8
mi*106 [Pas] 3
Propene
C3H6
6
Sulfur dioxide
Carbon dioxide
SO2
CO2
Carbon monoxide CO
lambda*103 [W/mK] 23.26 Hydrogen
H2
5.204 5.204
28.2
42.1
41.8
41
cp [kJ/kgK]
14.195 14.448 14.504 14.533 14.581 14.662 14.779 14.93 15.115
mi*106 [Pas]
8.4
lambda*103 [W/mK] 174.4
where is for flue gas:
• • •
t - temperature cp - specific heat mi - dynamic viscosity
•
lambda - thermal conductivity
10.3
12.1
13.9
15.4
16.9
18.3
19.6
21
216.3
258.2
300.1
341.9
383.8
452.7
467.5 509.4