APPENDIX C
FUNDAMENTALS OF PIPELINE HYDRAULICS
Section I. Physical Properties of Petroleum
TYPES OF PROPERTIES
Petroleum products have both chemical and physical properties or qualities. This manual is mainly concerned with kerosene, automotive gasoline, jet fuel, and diesel fuel. Both physical and chemical properties are of concern to the scheduler and dispatcher. However, only physical properties as they affect product storage and movement in pipelines are covered in this appendix. They include density, gravity, viscosity, compressibility, effect of temperature, and vapor pressure.
Density
All substances have weight. Their weight depends on the number and arrangement of molecules of which they are composed. Weight is a measure of the force of gravity. The weight of a definite mass of a substance varies slightly in different parts of the country because gravity varies. For this reason, weight and mass are not identical. Mass stays constant, but weight may not stay constant. The weight density or specific weight of a substance is its weight per unit volume. The term specific refers to a unit quantity. In the metric system of measurement, the mass of 1 cubic centimeter of water is 1 gram. Therefore, the density or specific weight of water is 1 gram per cubic centimeter. In the English system of measurement, the density or specific weight of water is expressed as 62.3 pounds per cubic foot. Specific volume is the space occupied by a unit quantity. In the metric system, 1 gram of water occupies 1 cubic centimeter. In the English system, 62.3 pounds of water occupies 1 cubic foot.
Gravity
Gravity is the attraction between matter and the earth's center. It is properly referred to as acceleration due to gravity, which is the change in speed of a body falling freely toward the earth. This change in speed is 32.2 feet per second. This means that during each second of fall, the speed increases 32.2 feet per second. Gravity is measured by weight. Petroleum operations are concerned with specific gravity and API gravity. Specific gravity and API gravity and formulas for converting one to the other are described below.
- Specific Gravity. Specific gravity is a means of comparing weights of substances. This is independent of the actual numerical value of the pull of gravity in any locality. Specific gravity is the ratio between the weight of a quantity or volume of a substance and the weight of an equal quantity of water. It is a relative measure of weight density compared with water. Solids and liquids are usually compared with water at its maximum density at 4° C. The specific gravity of water is 1. A substance of specific gravity 0.5 weighs half as much as water. A substance of specific gravity 5.0 weighs five times as much as water. Petroleum products moved by pipeline are lighter than water. Therefore, their specific gravities are fractions in a narrow numerical range. Specific gravity is measured with a hydrometer.
- API Gravity. The petroleum industry uses the API gravity scale almost exclusively to designate gravities of products. API gravities are based on reciprocals of specific gravities. They are whole numbers with a greater numerical spread. The API scale has a range of 0° to 100° . Water has a gravity of 10° API. This leaves a spread of 90° API between the heaviest and lightest petroleum products. API gravity is inversely proportionate to specific gravity. In other words, the higher the specific gravity, the heavier the product and the lower the API gravity. The lightest products have the highest API gravities.
- Formulas and Conversion Table. Formulas for converting specific gravity to API gravity and vice versa are given below. Table C-1 lists API gravity and corresponding specific gravity and weights at 60° F.
Degrees API gravity = |
141.5 |
-131.5 |
Specific gravity (60/60° F) = |
141.5 |
|
Table C-1. API gravity equivalents at 60° F
POUNDS PER |
BARRELS PER |
|||||||||
API SPECIFIC |
SPECIFIC |
US |
IMPERIAL |
BARREL |
LONG |
METRIC |
SHORT |
|||
1........ |
1.0679 |
8.895 |
10.683 |
373.59 |
5.996 |
5.901 |
5.353 |
|||
2........ |
1.0599 |
8.828 |
10.602 |
370.78 |
6.041 |
5.946 |
5.394 |
|||
3........ |
1.0520 |
8/762 |
10.523 |
368.00 |
6.087 |
5.991 |
5.435 |
|||
4........ |
1.0443 |
8.697 |
10.446 |
365.32 |
6.132 |
6.035 |
5.475 |
|||
5........ |
1.0368 |
8.634 |
10.369 |
362.63 |
6.177 |
6.080 |
5.516 |
|||
6........ |
1.0291 |
8.571 |
10.294 |
359.98 |
6.223 |
6.124 |
5.556 |
|||
7........ |
1.0217 |
8.509 |
10.219 |
357.38 |
6.268 |
6.169 |
5.596 |
|||
8........ |
1.0143 |
8.448 |
10.146 |
354.82 |
6.313 |
6.213 |
5.637 |
|||
9........ |
1.0071 |
8.388 |
10.074 |
352.30 |
6.359 |
6.258 |
5.677 |
|||
10a....... |
1.0000 |
8.328 |
10.002 |
349.78 |
6.404 |
6.303 |
5.718 |
|||
11......... |
0.9930 |
8.270 |
9.932 |
347.34 |
6.449 |
6.347 |
5.799 |
|||
12......... |
0.9861 |
8.212 |
9.863 |
344.90 |
6.495 |
6.392 |
5.799 |
|||
13......... |
0.9792 |
8.155 |
9.794 |
342.51 |
6.540 |
6.437 |
5.839 |
|||
14......... |
0.9725 |
8.099 |
9.727 |
340.16 |
6.585 |
6.481 |
5.880 |
|||
15......... |
0.9659 |
8.044 |
9.661 |
337.85 |
6.630 |
6.525 |
5.920 |
|||
16......... |
0.9593 |
7.989 |
9.595 |
335.54 |
6.676 |
6.570 |
5.961 |
|||
17......... |
0.9529 |
7.935 |
9.530 |
333.27 |
6.721 |
6.615 |
6.001 |
|||
18......... |
0.9465 |
7.882 |
9.466 |
331.04 |
6.766 |
6.660 |
6.042 |
|||
19......... |
0.9402 |
7.830 |
9.404 |
328.86 |
6.812 |
6.704 |
6.082 |
|||
20......... |
0.9340 |
7.778 |
9.341 |
326.68 |
6.857 |
6.749 |
6.122 |
|||
21......... |
0.9279 |
7.727 |
9.280 |
324.53 |
6.902 |
6.793 |
6.163 |
|||
22......... |
0.9218 |
7.676 |
9.219 |
322.39 |
6.948 |
6.838 |
6.204 |
|||
23......... |
0.9159 |
7.627 |
9.160 |
320.33 |
6.993 |
6.882 |
6.244 |
|||
24......... |
0.9100 |
7.578 |
9.101 |
318.28 |
7.038 |
6.927 |
6.284 |
|||
25......... |
0.9042 |
7.529 |
9.042 |
316.22 |
7.084 |
6.972 |
6.325 |
|||
26......... |
0.8984 |
7.481 |
8.985 |
314.20 |
7.129 |
7.017 |
6.365 |
|||
27...... |
0.8927 |
7.434 |
8.928 |
312.23 |
7.174 |
7.061 |
6.406 |
|||
28...... |
0.8871 |
7.387 |
8.872 |
310.25 |
7.220 |
7.106 |
6.446 |
|||
29...... |
0.8816 |
7.341 |
8.817 |
308.32 |
7.265 |
7.150 |
6.487 |
|||
30...... |
0.8762 |
7.296 |
8.762 |
306.43 |
7.310 |
7.194 |
6.527 |
|||
31...... |
0.8708 |
7.251 |
8.708 |
304.54 |
7.356 |
7.239 |
6.568 |
|||
32...... |
0.8654 |
7.206 |
8.654 |
302.65 |
7.401 |
7.284 |
6.603 |
|||
33...... |
0.8602 |
7.162 |
8.603 |
300.85 |
7.446 |
7.328 |
6.648 |
|||
34...... |
0.8550 |
7.119 |
8.550 |
299.00 |
7.492 |
7.373 |
6.689 |
|||
35...... |
0.8499 |
7.076 |
8.498 |
297.19 |
7.537 |
7.418 |
6.730 |
|||
36...... |
0.8448 |
7.034 |
8.448 |
295.43 |
7.582 |
7.462 |
6.770 |
|||
37...... |
0.8398 |
6.992 |
8.399 |
293.71 |
7.628 |
7.506 |
6.810 |
|||
38...... |
0.8348 |
6.951 |
8.348 |
291.94 |
7.673 |
7.552 |
6.851 |
|||
39...... |
0.8299 |
6.910 |
8.299 |
290.22 |
7.718 |
7.597 |
6.891 |
|||
40...... |
0.8251 |
6.870 |
8.251 |
288.54 |
7.764 |
7.641 |
6.931 |
|||
41...... |
0.8203 |
6.830 |
8.203 |
286.86 |
7.809 |
7.686 |
6.972 |
|||
42...... |
0.8156 |
6.790 |
8.155 |
285.18 |
7.854 |
7.731 |
7.013 |
|||
43...... |
0.8109 |
6.751 |
8.109 |
283.58 |
7.900 |
7.774 |
7.053 |
|||
44...... |
0.8063 |
6.713 |
8.062 |
281.95 |
7.945 |
7.819 |
7.093 |
|||
45...... |
0.0817 |
6.675 |
8.017 |
280.35 |
7.990 |
7.864 |
7.134 |
|||
46...... |
0.7972 |
6.637 |
7.971 |
278.75 |
8.036 |
7.909 |
7.175 |
|||
47...... |
0.7927 |
6.600 |
7.927 |
277.20 |
8.081 |
7.953 |
7.215 |
|||
48...... |
0.7883 |
6.563 |
7.882 |
275.65 |
8.126 |
7.998 |
7.256 |
|||
49...... |
0.7839 |
6.527 |
7.838 |
274.09 |
8.172 |
8.043 |
7.297 |
|||
50...... |
0.7796 |
6.491 |
7.794 |
272.58 |
8.217 |
8.088 |
7.337 |
|||
51...... |
0.7753 |
6.455 |
7.752 |
271.11 |
8.262 |
8.132 |
7.377 |
|||
52...... |
0.7711 |
6.420 |
7.710 |
269.64 |
8.308 |
8.176 |
7.417 |
|||
53...... |
0.7669 |
6.385 |
7.668 |
268.17 |
8.353 |
8.221 |
7.458 |
|||
54...... |
0.7628 |
6.350 |
7.626 |
266.70 |
8.398 |
8.266 |
7.499 |
|||
55...... |
0.7587 |
6.316 |
7.586 |
265.27 |
8.444 |
8.130 |
7.539 |
|||
56...... |
0.7547 |
6.283 |
7.546 |
263.89 |
8.489 |
8.354 |
7.579 |
|||
57...... |
0.7507 |
6.249 |
7.505 |
262.46 |
8.534 |
8.400 |
7.620 |
|||
58...... |
0.7467 |
6.216 |
7.465 |
261.07 |
8.850 |
8.444 |
7.661 |
|||
59...... |
0.7428 |
6.183 |
7.427 |
259.73 |
8.625 |
8.488 |
7.700 |
|||
60...... |
0.7389 |
6.151 |
7.387 |
258.34 |
7.670 |
8.534 |
7.742 |
|||
61...... |
0.7351 |
6.119 |
7.349 |
257.00 |
8.716 |
8.578 |
7.782 |
|||
62...... |
0.7313 |
6.087 |
7.310 |
255.65 |
8.761 |
8.623 |
7.823 |
|||
63...... |
0.7275 |
6.056 |
7.273 |
254.35 |
8.807 |
8.668 |
7.863 |
|||
64...... |
0.7238 |
6.025 |
7.236 |
253.05 |
8.852 |
8.712 |
7.904 |
|||
65...... |
0.7201 |
5.994 |
7.199 |
251.75 |
8.897 |
8.757 |
7.944 |
|||
66...... |
0.7165 |
5.964 |
7.163 |
250.49 |
8.943 |
8.801 |
7.984 |
|||
67...... |
0.7128 |
5.934 |
7.127 |
249.23 |
8.988 |
8.846 |
8.025 |
|||
68...... |
0.7093 |
5.904 |
7.091 |
247.97 |
9.033 |
8.891 |
8.065 |
|||
69...... |
0.7057 |
5.875 |
7.055 |
246.71 |
9.079 |
8.936 |
8.107 |
|||
70...... |
0.7022 |
5.845 |
7.020 |
245.49 |
9.125 |
8.980 |
8.147 |
|||
71...... |
0.6988 |
5.816 |
6.986 |
244.31 |
9.169 |
9.024 |
8.187 |
|||
72...... |
0.6953 |
5.788 |
6.951 |
243.10 |
9.215 |
9.069 |
8.227 |
|||
73...... |
0.6919 |
5.759 |
6.917 |
241.88 |
9.260 |
9.114 |
8.269 |
|||
74...... |
0.6886 |
5.731 |
6.883 |
240.70 |
9.305 |
9.159 |
8.309 |
|||
75...... |
0.6852 |
5.704 |
6.849 |
239.53 |
9.351 |
9.204 |
8.350 |
|||
76...... |
0.6819 |
5.676 |
6.817 |
238.39 |
9.396 |
9.248 |
8.390 |
|||
77...... |
0.6787 |
5.649 |
6.784 |
237.26 |
9.442 |
9.292 |
8.430 |
|||
78...... |
0.6754 |
5.622 |
6.752 |
236.12 |
9.487 |
9.337 |
8.470 |
|||
79...... |
0.6722 |
5.595 |
6.720 |
234.99 |
9.532 |
9.382 |
8.511 |
|||
80...... |
0.6690 |
5.569 |
6.687 |
238.86 |
9.578 |
9.427 |
8.552 |
|||
81...... |
0.6659 |
5.542 |
6.656 |
232.76 |
9.623 |
9.472 |
8.593 |
|||
82...... |
0.6628 |
5.516 |
6.624 |
231.67 |
9.668 |
9.516 |
8.633 |
|||
83...... |
0.6597 |
5.490 |
6.595 |
230.62 |
9.714 |
9.559 |
8.672 |
|||
84...... |
0.6566 |
5.465 |
6.563 |
229.53 |
9.759 |
9.605 |
8.713 |
|||
85...... |
0.6536 |
5.440 |
6.533 |
228.48 |
9.805 |
9.649 |
8.754 |
|||
86...... |
0.6506 |
5.415 |
6.503 |
227.43 |
9.850 |
9.694 |
8.794 |
|||
87...... |
0.7476 |
5.390 |
6.473 |
226.38 |
9.895 |
9.738 |
8.835 |
|||
88...... |
0.6446 |
5.365 |
6.443 |
225.33 |
9.941 |
9.784 |
8.876 |
|||
89...... |
0.6417 |
5.341 |
6.415 |
224.32 |
9.986 |
9.828 |
8.916 |
|||
90...... |
0.6388 |
5.317 |
6.385 |
223.27 |
10.031 |
9.874 |
8.957 |
|||
91...... |
0.6360 |
5.293 |
6.357 |
222.31 |
10.077 |
9.917 |
8.996 |
|||
92...... |
0.6331 |
5.269 |
6.328 |
221.30 |
10.122 |
9.962 |
9.038 |
|||
93...... |
0.6303 |
5.245 |
6.300 |
220.33 |
10.168 |
10.006 |
9.077 |
|||
94...... |
0.6275 |
5.222 |
6.273 |
219.37 |
10.213 |
10.050 |
9.117 |
|||
aWater (H2O AT 60oF) |
VISCOSITY
Viscosity is the internal resistance of a liquid to flow. A liquid is said to be viscous if it is sluggish or thick. Lubricating oil must be viscous enough to maintain a lubricating film under all operating conditions. However, it must not be so viscous that it becomes a drag or causes a power loss. Absolute viscosity is a measure of the force required to produce motion. The unit of force in the metric system is called the poise. One poise is equal to 100 centipoises. Viscosity is measured by noting the time in seconds for a standard amount of product to flow through a viscosimeter. The Saybolt Universal instrument is the type of viscosimeter commonly used for such measurements. A more accurate instrument for measuring viscosity is the Ubbelohde viscosimeter. Conversions from kinematic to Saybolt viscosity can be taken from the ASTM table (Table C-2).
Table C-2. Kinematic viscosity converted to Saybolt Universal viscosity
KINEMATAIC
|
EQUIVALENT SAYBOLT
|
KINEMATAIC
|
EQUIVALENT SAYBOLT
|
||
AT 100°F |
AT 210°F |
AT 100°F |
AT 210°F |
||
2........ |
32.6 |
32.9 |
27 |
128.1 |
129.0 |
2.5....... |
34.4 |
34.7 |
28 |
132.5 |
133.4 |
3........ |
36.0 |
36.3 |
29 |
136.9 |
137.9 |
3.5....... |
37.6 |
37.9 |
30 |
141.3 |
142.3 |
4........ |
39.1 |
39.4 |
31 |
145.7 |
146.8 |
4.5....... |
40.8 |
41.0 |
32 |
150.2 |
151.2 |
5........ |
42.4 |
42.7 |
33 |
154.7 |
155.8 |
6....... |
45.6 |
45.9 |
34 |
159.2 |
160.3 |
7........ |
48.8 |
49.1 |
35 |
163.7 |
164.9 |
8........ |
52.1 |
52.5 |
36 |
168.2 |
169.4 |
9........ |
55.5 |
55.9 |
37 |
172.7 |
173.9 |
10...... |
58.9 |
59.3 |
38 |
177.3 |
178.5 |
11....... |
62.4 |
62.9 |
39 |
181.8 |
183.0 |
12....... |
66.0 |
66.5 |
40 |
186.3 |
187.6 |
13....... |
69.8 |
70.3 |
41 |
190.8 |
192.1 |
14....... |
73.6 |
74.1 |
42 |
195.3 |
196.7 |
15....... |
77.4 |
77.9 |
43 |
199.8 |
201.2 |
16....... |
81.3 |
81.9 |
44 |
204.4 |
205.9 |
17....... |
85.3 |
85.9 |
45 |
209.1 |
210.5 |
18....... |
89.4 |
90.1 |
46 |
213.7 |
215.2 |
19....... |
93.6 |
94.2 |
47 |
218.3 |
219.8 |
20....... |
97.8 |
98.5 |
48 |
222.9 |
224.5 |
21....... |
102.0 |
102.8 |
49 |
227.5 |
229.1 |
22....... |
106.4 |
107.1 |
50 |
232.1 |
233.8 |
23....... |
110.7 |
111.4 |
55 |
255.2 |
257.0 |
24....... |
115.0 |
115.8 |
60 |
278.3 |
280.2 |
25....... |
119.3 |
120.1 |
65 |
301.4 |
303.5 |
26....... |
123.7 |
124.5 |
70 |
324.4 |
326.7 |
Over 70..... |
Saybolt |
Saybolt |
|||
Note: To obtain the Saybolt Universal viscosity equivalent to a kinematic viscosity determined at tF, multiply the equivalent Saybolt Universal viscosity at 100F by 1+(t - 100) 0.000034: for example, 10cSt at 210°F are equivalent to 58.9 x 1.0070 or 59.3 seconds Saybolt Universal at 210°F. |
Compressibility
All fluids are compressible to an extent. That is, they can be made to occupy less space by increasing the pressure or decreasing the temperature. Liquids have perfect elasticity. They return to their original volume when the pressure is lowered or the temperature is increased. Products of the highest API gravity have the greatest compressibility. They can generate the highest surge pressure, known as hydraulic shock or water hammer. Products of high API gravity can also be transferred at the highest rate of flow. This also increases the possibility of surge pressure. Surge pressure must be avoided. Apart from surge pressure, compressibility has little significance in military dispatching of petroleum products.
TEMPERATURE
The effects of product temperature and its measurement and correction are described below.
Effects
Product temperature affects all of the properties discussed above. Volume, API gravity, compressibility, and volatility increase with temperature. Density, specific gravity, and viscosity decrease when the temperature increases. Pipeline throughput is higher in summer than in winter and requires less power. A pipeline heated by the sun delivers a greater volume. The API gravity is also higher in a pipeline than in the cool interior of a storage tank. Lubricating oil may be too thick to lubricate an engine properly when the engine is started on a cold morning. The same engine oil may thin out under operating temperatures. The change in viscosity with temperature is called viscosity index. It varies from product to product.
Measurements
Product is measured and tested many times between manufacture and consumption. Input stations report to the dispatcher temperatures and quantities pumped every hour. Takeoff stations report temperatures and quantities received every hour. Quantities are determined by gaging as shown in Tables C-3 and C-4, page C-6. Because of the effects of temperature on volume and gravity, all measurements are corrected to 60° F.
Table C-3. Gage data for military bolted tanks (capacities shown in barrels of 42 gallons)
DEPTH |
100 bbla |
250 bbla |
500 bbla |
1,000 bbla |
10,000 bblb |
¼ in |
0.24 |
0.69 |
1.35 |
2.57 |
8.81 |
½ in |
.49 |
1.38 |
2.70 |
5.15 |
17.62 |
¾ in |
.73 |
2.07 |
4.06 |
7.72 |
26.43 |
1 in |
.98 |
2.76 |
5.41 |
10.30 |
35.23 |
2 in |
1.97 |
5.52 |
10.82 |
20.59 |
70.47 |
3 in |
2.96 |
8.28 |
16.23 |
30.89 |
105.70 |
4 in |
3.95 |
11.04 |
21.64 |
41.18 |
140.94 |
5 in |
4.94 |
13.80 |
27.05 |
51.48 |
176.17 |
6 in |
5.93 |
16.56 |
32.46 |
61.77 |
211.41 |
7 in |
6.92 |
19.32 |
37.87 |
72.07 |
246.64 |
8 in |
7.91 |
22.07 |
43.28 |
82.36 |
281.88 |
9 in |
8.90 |
24.83 |
46.68 |
92.66 |
317.11 |
10 in |
9.89 |
27.59 |
54.09 |
102.96 |
352.35 |
11 in |
10.88 |
30.35 |
59.50 |
113.25 |
387.58 |
1 ft 0 in |
11.87 |
33.11 |
64.91 |
123.56 |
422.82 |
2 ft 0 in |
23.76 |
66.22 |
129.83 |
247.09 |
845.64 |
3 ft 0 in |
35.66 |
99.34 |
194.74 |
370.64 |
1,268.46 |
4 ft 0 in |
47.54 |
132.45 |
259.65 |
494.19 |
1,691.28 |
5 ft 0 in |
59.43 |
165.56 |
324.56 |
617.74 |
2,114.09 |
6 ft 0 in |
71.32 |
198.67 |
389.48 |
741.28 |
2,536.91 |
7 ft 0 in |
83.21 |
231.79 |
454.39 |
864.38 |
2,959.73 |
8 ft 0 in |
95.10 |
c264.90 |
c519.30 |
988.38 |
3,382.55 |
9 ft 0 in |
106.99 |
c298.01 |
584.22 |
c1,111.93 |
3,805.37 |
10 ft 0 in |
118.88 |
331.12 |
649.13 |
1,235.47 |
4,228.19 |
11 ft 0 in |
130.77 |
364.24 |
714.04 |
1,359.02 |
4,651.01 |
12 ft 0 in |
142.66 |
397.35 |
778.96 |
1,482.57 |
5,073.83 |
13 ft 0 in |
154.55 |
430.46 |
843,87 |
1,606.12 |
5,496.64 |
14 ft 0 in |
166.44 |
463.57 |
908.78 |
1,729.66 |
5,919.46 |
15 ft 0 in |
178.33 |
496.69 |
973.69 |
1,853.29 |
6,342.28 |
16 ft 0 in |
190.22 |
529.80 |
1,038.61 |
1,976.76 |
6,765.10 |
17 ft 0 in |
..... |
.... |
.... |
2,100.30 |
7,187.92 |
18 ft 0 in |
..... |
.... |
.... |
2,223.85 |
7,610.74 |
19 ft 0 in |
..... |
.... |
.... |
2,347.40 |
8,033.56 |
20 ft 0 in |
..... |
.... |
.... |
2,470.95 |
8,456.38 |
21 ft 0 in |
..... |
.... |
.... |
2,594.49 |
8,879.19 |
22 ft 0 in |
..... |
.... |
.... |
2,718.04 |
9,302.01 |
23 ft 0 in |
..... |
.... |
.... |
2,841.59 |
9,724.83 |
24 ft 0 in |
..... |
.... |
.... |
2,965.13 |
10,147.65 |
a One-ring tank.
|
Table C-4. Deadwood for military bolted tanks (capacities are in barrels of 42 gallons)
DEPTH |
100 bbla |
250 bbla |
500 bbla |
1,000 bbla |
10,000 bblb |
1 ft 0 in |
0.007 |
0.008 |
0.010 |
0.030 |
0.055 |
2 ft 0 in |
.013 |
.016 |
.020 |
.060 |
.110 |
3 ft 0 in |
.019 |
.024 |
.030 |
.089 |
.164 |
4 ft 0 in |
.026 |
.032 |
.40 |
.119 |
.217 |
5 ft 0 in |
.031 |
.039 |
.048 |
.145 |
.279 |
6 ft 0 in |
.036 |
.046 |
.057 |
.169 |
.340 |
7 ft 0 in |
.042 |
.053 |
.065 |
.195 |
.405 |
8 ft 0 in |
.047 |
.058 |
.073 |
.219 |
.467 |
9 ft 0 in |
.052 |
.066 |
.081 |
.243 |
.508 |
10 ft 0 in |
.058 |
.073 |
.089 |
.268 |
.548 |
11 ft 0 in |
.063 |
.079 |
.098 |
.292 |
.586 |
12 ft 0 in |
.069 |
.086 |
.105 |
.317 |
.624 |
13 ft 0 in |
.074 |
.093 |
.113 |
.340 |
.665 |
14 ft 0 in |
.079 |
.100 |
.122 |
.366 |
.700 |
15 ft 0 in |
.084 |
.106 |
.129 |
.390 |
.740 |
16 ft 0 in |
.090 |
.113 |
.137 |
.416 |
.779 |
17 ft 0 in |
..... |
.... |
.... |
.441 |
.817 |
18 ft 0 in |
..... |
.... |
.... |
.464 |
.855 |
19 ft 0 in |
..... |
.... |
.... |
.490 |
.893 |
20 ft 0 in |
..... |
.... |
.... |
.521 |
.933 |
21 ft 0 in |
..... |
.... |
.... |
.538 |
.972 |
22 ft 0 in |
..... |
.... |
.... |
.562 |
1.006 |
23 ft 0 in |
..... |
.... |
.... |
.586 |
1.100 |
24 ft 0 in |
..... |
.... |
.... |
.690 |
1.368 |
a One-ring tank.
|
Corrections
Volume correction to 60° F requires observation of both gravity and temperature. They should be taken as close to the same time as possible. Combination hydrometers and thermometers make this easier. If specific gravity is taken, it must be converted to API gravity. Gravity at the observed temperature is corrected to 60° F. Volume correction factors are based on true or corrected gravity. Corrections are made according to the API/ASTM-IP Petroleum Measurement Table (Tables 5B and 6B) and DA Pam 710-2-2. Table 5B gives factors for correcting observed API gravity to true gravity at 60° F. Table 6B gives correction factors for each degree or half degree of API gravity and each degree or half degree of temperature. Gravity must be corrected to 60° F to ensure that the multiplier is selected from the proper group. This is most important near the ends of the eight gravity ranges. The multiplier is a ratio volume at 60° F to volume at the observed temperature. If the observed temperature is higher than 60° F, the multiplier is less than 1 and the corrected volume will be smaller. If observed temperature is less than 60° F, the multiplier is less than 1 and the corrected volume will be larger.
Section II. Flow in Pipelines
HYDRAULICS
The principles of hydraulics govern flow in pipelines. Hydraulics is the branch of science that deals with the behavior of liquids. It also deals with the equipment required to raise liquids to higher elevations and to transfer them from place to place. The broad subject includes the pressure and the equilibrium of liquids at rest (hydrokinetics), as in an operating pipeline, and forces exerted on liquids by objects in motion (hydrodynamics), as in pumping equipment.
PRESSURE
Pressure is the main element in pipeline hydraulics. All forces producing pipeline flow and those opposing it can be measured in terms of pressure or head. Coupled military pipelines are low-pressure systems that operate at pressures of not more than 600 PSI. The low pressure requires closer pump station spacing than in commercial pipeline. Pump stations are spaced about 12 to16 miles apart in military systems on level terrain. Welded lines constructed for the military operate at higher pressures. The two types of pressure in a pipeline are static and dynamic.
Static Pressure
Static pressure is a measure of pressure in liquids at rest. At any level in any size or shape of container, static pressure depends solely upon the vertical height of liquid above that level. Unit pressure at the bottom of all containers shown in Figure C-1, is the same, 1 PSI. A column of water 1 inch square and about 27 inches high weighs 1 pound. The force of 1 pound acts on an area of 1 square inch in the first container. The second container holds 4 pounds of water distributed over 4 square inches. The third container holds 16 pounds distributed over 16 square inches. The fourth holds 64 pounds distributed over 64 square inches. Total pressure varies at the bottom of all containers in Figure C-1, and Figure C-2, but unit pressure is the same, 1 PSI. The height of water in all the containers, 27 inches or 2.31 feet, is the head required to produce a pressure of 1 PSI. Static pressure in any column of water is the head in feet divided by 2.31 or multiplied by 0.433 (Table C-5, page C-9). Static pressure is proportionally less in a petroleum product because of its lower specific gravity. The formulas for converting head to pressure and vice versa are as follows:
Pressure (PSI) = |
head (in feet) x specific gravity |
|
|
or | |
Pressure (PSI) = 0.433 x head (in feet) x specific gravity | |
or | |
Head (in feet) = |
PSI |
|
Figure C-1. Pressure in containers of different dimensions
Figure C-2. Pressure in irregularly shaped containers
Table C-5. API gravity, corresponding specific gravity, weights, and pressure at 60°F
API GRAVITY |
SPECIFIC |
POUNDS PER |
FEET PER PSI |
PSI PER FOOT |
10 |
1.0000 |
62.30 |
2.31 |
0.433 |
15 |
.9659 |
60.17 |
2.39 |
.418 |
20 |
.9340 |
58.18 |
2.48 |
.404 |
25 |
.9042 |
56.32 |
2.56 |
.391 |
26 |
.8984 |
55.96 |
2.57 |
.389 |
27 |
.8927 |
55.61 |
2.59 |
.386 |
28 |
.8871 |
55.26 |
2.61 |
.384 |
29 |
.8816 |
54.92 |
2.62 |
.381 |
30 |
.8762 |
54.58 |
2.64 |
.379 |
31 |
.8708 |
54.24 |
2.66 |
.377 |
32 |
.8654 |
53.90 |
2.67 |
.374 |
33 |
.8602 |
53.58 |
2.69 |
.372 |
34 |
.8550 |
53.25 |
2.70 |
.370 |
35 |
.8498 |
52.93 |
2.72 |
.368 |
36 |
.8448 |
52.62 |
2.74 |
.365 |
37 |
.8398 |
52.31 |
2.75 |
.363 |
38 |
.8348 |
52.00 |
2.77 |
.361 |
39 |
.8299 |
51.69 |
2.79 |
.359 |
40 |
.8251 |
51.39 |
2.80 |
.357 |
41 |
.8203 |
51.09 |
2.82 |
.355 |
42 |
.8155 |
50.79 |
2.84 |
.353 |
43 |
.8109 |
50.51 |
2.85 |
.351 |
44 |
.8063 |
50.22 |
2.87 |
.349 |
45 |
.8017 |
49.93 |
2.88 |
.347 |
46 |
.7972 |
49.65 |
2.90 |
.345 |
47 |
.7927 |
49.37 |
2.92 |
.343 |
48 |
.7883 |
49.10 |
2.93 |
.341 |
49 |
.7839 |
48.82 |
2.95 |
.339 |
50 |
.7796 |
48.55 |
2.97 |
.337 |
51 |
.7753 |
48.29 |
2.98 |
.335 |
52 |
.7711 |
48.02 |
3.00 |
.334 |
53 |
.7669 |
47.76 |
3.02 |
.332 |
54 |
.7628 |
47.50 |
3.03 |
.330 |
55 |
.7587 |
47.25 |
3.05 |
.328 |
56 |
.7547 |
47.00 |
3.06 |
.326 |
57 |
.7507 |
46.75 |
3.08 |
.325 |
58 |
.7467 |
46.50 |
3.10 |
.323 |
59 |
.7428 |
46.26 |
3.11 |
.321 |
60 |
.7389 |
46.01 |
3.13 |
.320 |
61 |
.7351 |
45.77 |
3.15 |
.318 |
62 |
.7313 |
45.53 |
3.16 |
.316 |
63 |
.7275 |
45.30 |
3.18 |
.315 |
64 |
.7238 |
45.07 |
3.19 |
.313 |
65 |
.7201 |
44.84 |
3.21 |
.311 |
66 |
.7165 |
44.61 |
3.22 |
.210 |
67 |
.7128 |
44.39 |
3.24 |
.308 |
68 |
.7093 |
44.16 |
3.26 |
.307 |
69 |
.7057 |
43.94 |
3.27 |
.305 |
70 |
.7022 |
43.72 |
3.29 |
.304 |
71 |
,6988 |
43.51 |
3.30 |
.302 |
72 |
.6953 |
43.30 |
3.32 |
.301 |
73 |
.6919 |
43.08 |
3.34 |
.299 |
74 |
.6886 |
42.87 |
3.35 |
.298 |
75 |
.6852 |
42.66 |
3.37 |
.296 |
Dynamic Pressure
Dynamic pressure or head is a measure of pressure in liquids in motion. Dynamic head is also a measure of potential energy or energy of position. Figure C-3, shows the relationship between static head and dynamic head. Static head at ground level behind the nozzle is measured by the vertical height of liquid in the tank above the ground. When liquid starts to flow down the pipe, it loses static head, but it gains in dynamic head. Potential energy becomes kinetic energy or energy in motion. Dynamic head or velocity is greatest at ground level where the stream changes direction and starts to rise. Dynamic head decreases after that until all velocity is lost. Meanwhile, the stream regains some portion of its initial static head and final static head is the head loss because of friction and change in direction. In other words, dynamic head is the static head required to accelerate the stream to its flowing velocity. It is the elevation to which a pump can push a column of liquid.
Figure C-3. Relationship between static head and dynamic head
Pascal's Law
Pascal's law states that pressure, applied to the surface of a liquid, is transmitted equally in all directions through the liquid. It adds that, at any point, pressure acts at right angles to the confining container with undiminished intensity. Figure C-4, shows Pascal's law and the effect of total pressure. Unit pressure is the same on both pistons, 10 PSI. This pressure is transmitted throughout the liquid. Therefore, a total pressure of 30 pounds on one piston can exert a total pressure of 1,000 pounds on the other. This principle is used in hydraulic presses, jacks, and brakes.
Atmospheric Pressure
Atmospheric pressure is caused by the weight of air above the earth. It is the same everywhere at any given elevation. Atmospheric pressure is similar to static pressure in liquids. The height of a column of air depends upon the height of the column. It is measured by the height in inches it raises a column of mercury in a barometer. Atmospheric pressure is 14.695 PSI at sea level and proportionally less at higher altitudes. Maximum suction lift of centrifugal pumps at sea level is 33(+) feet of water (14.695 PSI x 2.31). Pump engines are affected at elevations greater than 3,000 feet because of thinner air. This same condition lowers atmospheric pressure. Design loads on pumps are usually reduced by 4 percent for each 1,000 feet of elevation above 3,000 feet. Normal suction pressure of 20 PSI is based on a design fuel of 0.725 specific gravity. This pressure should be increased to 30 PSI for elevations over 5,000 feet.
Figure C-4. Illustration of Pascal's law
Vacuum
A vacuum is created when pressure is reduced below atmospheric level. The theoretical limit of pressure reduction is absolute zero or perfect vacuum. Vacuums are measured as absolute pressure in inches of mercury. Pump suction reduces atmospheric pressure at the point of intake. This allows atmospheric pressure on the source of supply to push liquids into the pump. Figure C-5 shows the relationship between atmospheric pressure, gage pressure, vacuum, and absolute pressure.
Figure C-5. Interrelationship of atmospheric pressure, gage pressure, vacuum, and absolute pressure
Vapor Pressure
All liquids, especially light petroleum products, tend to vaporize. This results from motion of the molecules of which they are composed. Motion of molecules near the surface causes some to escape into the air. The tendency to vaporize is called volatility. Volatility increases with temperature and decreases with pressure. Vapor pressure is formed when a vaporizing liquid is confined in a closed container like that used in the Reid vapor pressure test. The temperature at which vapor pressure is the boiling point of the liquid. For this reason, liquids boil at lower temperatures at high elevations than at sea level. Vapor pressure reduces the effect of atmospheric pressure acting on the liquid. Maximum net suction lift is reduced accordingly. For this reason, pump suction pressure always must be greater than the vapor pressure of the product. Normal suction pressure of 20 PSI should be increased to 30 PSI for operating temperatures over 100° F.
NATURE OF FLOW
The two types of flow are laminar and turbulent. They are covered in Chapter 9. Liquids flow in pipelines because of gravity or pump action. In both cases, they flow because of pressure. Pressure is supplied by weight of the liquid in gravity flow and by pump action in discharge flow. While pressure and head are almost synonymous, they are actually proportional to each other.
RESISTANCE OF FLOW
Flow in a pipeline continues until the head producing it has been lost. The loss of head or the difference between pressure at the source and at any point downstream is caused by factors that resist flow. The main factors that resist flow are friction of the pipe walls and viscosity of the liquid. Friction loss calculations are covered in detail in FM 5-482, Chapter 4. To calculate friction loss for JP-8, use Table C-6, and Figure C-6. Less important factors in flow resistance include:
- Entrance to the pipe.
- Sudden changes in cross-sectional area or direction of flow.
- Resistance of valves and fittings.
- Passage through equipment, such as meters and traps.
- Corrosion or deposits in the line.
RATE OF FLOW
The rate of flow depends on pump pressure and differences in elevation. It also depends on gravity and viscosity of the product, diameter and length of the pipe, and roughness of the pipe.
Pressure
There is friction between the liquid and the pipe walls. The pressure needed to overcome this resistance is expressed as pressure drop or loss in pounds per square inch per mile of pipe as shown in Figure C-7. The pressure needed to overcome the resistance of valves and fittings is similarly expressed in equivalent lengths of pipe as shown in Figure C-8, and Table C-6. The total pressure needed to overcome all resistance in the line is pressure drop per mile times length of the line in miles. There is a direct relationship between pressure and rate of flow. This is shown by the fact that about double the pressure is needed to increase throughput by one half as shown in Table C-8, page C-16.
Figure C-6. Kinematic viscosities for common military fuels
Table C-6. Pipe lengths equivalent to lubricated plug valves
Nominal Size (inches) |
125-POUND CAST IRON AND 150-POUND NONFERROUS METAL |
250-POUND CAST IRON |
150-POUND STEEL |
300-POUND STEEL |
|||||||
Regular |
Short |
Venturi |
Regular |
Venturi |
Regular |
Short |
Venturi |
Regular |
Short |
Venturi |
|
6 |
12 |
44 |
36 |
12 |
36 |
9.6 |
14.4 |
36 |
... |
42 |
... |
8 |
18 |
54 |
54 |
18 |
54 |
12.0 |
48.0 |
54 |
9.6 |
54 |
54 |
10 |
24 |
60 |
60 |
24 |
60 |
.... |
54.0 |
60 |
... |
66 |
60 |
12 |
30 |
72 |
78 |
... |
78 |
... |
72.0 |
84 |
... |
... |
77 |
Table C-7. Relationship of pressure and quantity with length and diameter constant
RELATIVE |
INCREASE |
RELATIVE |
INCREASE IN QUANTITY |
RELATIVE |
DECREASE IN |
RELATIVE |
DECREASE IN QUANTITY |
1.00 |
..... |
1.00 |
...... |
1.00 |
...... |
1.00 |
...... |
1.02 |
2 |
1.01 |
1 |
.98 |
2 |
.99 |
1 |
1.04 |
4 |
1.02 |
2 |
.96 |
4 |
.98 |
2 |
1.06 |
6 |
1.03 |
3 |
.94 |
6 |
.96 |
4 |
1.08 |
8 |
1.05 |
5 |
.92 |
8 |
.95 |
5 |
1.10 |
10 |
1.06 |
6 |
.90 |
10 |
.94 |
6 |
1.12 |
12 |
1.07 |
7 |
.88 |
12 |
.93 |
7 |
1.15 |
15 |
1.08 |
8 |
.85 |
15 |
.91 |
9 |
1.20 |
20 |
1.11 |
11 |
.80 |
20 |
.88 |
12 |
1.25 |
25 |
1.14 |
14 |
.75 |
25 |
.85 |
15 |
1.30 |
30 |
1.16 |
16 |
.70 |
30 |
.81 |
19 |
1.40 |
40 |
1.22 |
22 |
.60 |
40 |
.74 |
26 |
1.50 |
50 |
1.26 |
26 |
50 |
50 |
.67 |
33 |
1.75 |
75 |
1.38 |
38 |
.40 |
60 |
.58 |
42 |
2.00 |
100 |
1.49 |
49 |
.30 |
70 |
.49 |
51 |
Figure C-7. Pressure loss due to friction in pipe
Figure C-8. Pipe lengths equivalent to valves and fittings
Elevation
Pressure needed to overcome friction is not the total pressure supplied if the product is to be pumped over a hill higher than the pump. The pressure equivalent of the difference in elevation in feet must be added to the pressure needed to overcome friction. If the liquid is to flow downhill from the pump, the difference in elevation can be subtracted. Otherwise, the liquid will flow proportionally farther at the same pump pressure. Elevation or static pressure acts at all times on a filled line whether the liquid is flowing or not.
Gravity
Specific gravity of the product is important because the liquid being moved has weight. The greater the specific gravity, or the lower the API gravity, the greater must be the pump pressure to move it. As heavier products are pumped in the line, pressure must be increased to keep the same flow rate. At the same pressure, flow rate falls off to suit the heaviest product being pumped. Observed gravity should be used in rate-of-flow computations instead of true gravity. This is because the computation will be concerned with an actual, not theoretical, condition. Changing from 40 API gravity to 60 API gravity lessens pressure requirements 10 percent. At the same pressure, changing from 40 API gravity to 60 API gravity increases rate of flow about 7 percent.
Viscosity
Viscosity and specific gravity of product affect pump pressure in the same way. As more viscous products are pumped, pressure must be increased to keep the same rate of flow as shown in Table C-8. Both gravity and viscosity vary with temperature. Therefore, locations with temperature differences of about 50° F require 10 to 20 percent higher pumping pressures in winter.
Table C-8. Relationship of viscosity, quantity, and pressure
VISCOSITYa |
RELATIVE QUANTITY WITH |
VISCOSITYa |
RELATIVE PRESSURE WITH |
||
Ab |
Bc |
Ab |
Bc |
||
35 |
120 |
100 |
35 |
73 |
100 |
40 |
110 |
91 |
40 |
85 |
117 |
45 |
104 |
86 |
45 |
90 |
128 |
50 |
100 |
83 |
50 |
100 |
137 |
55 |
97 |
81 |
55 |
105 |
144 |
60 |
95 |
79 |
60 |
109 |
150 |
70 |
91 |
76 |
70 |
117 |
161 |
80 |
89 |
74 |
80 |
123 |
168 |
90 |
87 |
72 |
90 |
128 |
175 |
100 |
85 |
71 |
100 |
132 |
182 |
125 |
82 |
68 |
125 |
142 |
194 |
150 |
79 |
66 |
150 |
150 |
205 |
200 |
75 |
63 |
200 |
162 |
222 |
300 |
71 |
59 |
300 |
182 |
249 |
a Viscosity in Saybolt Universal seconds.
|
Diameter of Pipe
The pressure needed to pump at a given flow rate decreases rapidly as pipe diameter increases. It requires about 85 feet of pressure drop per mile to pump gasoline at the rate of 550 GPM through a 6.407-inch pipeline. Only about 22 feet of pressure drop are needed to pump at the same rate through 8.407-inch pipeline as shown in Figure C-6. The decrease is about 74 percent. The same rate of flow requires about 600 feet of pressure drop for 4.344-inch pipeline. This is an increase of more than 500 percent. At any given pressure, throughput may be increased about threefold by increasing the pipe diameter 50 percent.
Length of pipe
Required pumping pressure increases directly with distance pumped. In other words, pressure drop per mile is proportional to distance pumped. If distance is doubled, pressure must be doubled. If pressure stays constant, rate of flow varies inversely as the approximate square root of length. For example, if station spacing is decreased by one half, flow rate will increase by about one half.
Roughness of pipe
Required pumping pressure increases directly with roughness of pipe For this reason, scrapers and corrosion inhibitors must be used to keep the pipeline in good operating condition.
Section III. Examples of Flow
HYDRAULIC GRADIENT
Figure C-9 shows what is meant by hydraulic gradient. The figure shows a tank with a pipeline of uniform size and grade connected at point A and discharging into the atmosphere at point B. Vertical pipes that open to the atmosphere have been connected at points X, Y, and Z. The tank is filled with product to a height of 10 feet above A and B. The hydraulic gradient exists only under conditions of flow. It is assumed that the level of product in the tank stays the same when flow begins. Product rises in each of the vertical pipes to a height (D, E, and F) that represents the remaining feet of head at X, Y, and Z. The head that has been lost at each point is proportional to the length of pipe through which product has flowed. Pressure head is lost uniformly from A to B. This uniform loss of head is the hydraulic gradient. It is shown by the line connecting points C, D, E, F, and B.
Figure C-9. Hydraulic gradient
DOWNHILL FLOW
Figure C-10, shows a situation in which the product flows downhill. Conditions are the same as in Figure C-8, except that point B is 10 feet below the tank connection A. This change increases the head to 20 feet. The new C to B line is the hydraulic gradient. This gradient is steeper than in Figure C-8. The rate of flow or velocity is also greater.
Figure C-10. Downhill flow
UPHILL FLOW
Figure C-11, shows a situation in which product flows uphill. The point of discharge B is 5 feet above the tank outlet A. Effective head has been reduced to 5 feet. The hydraulic gradient is not as steep as that in Figure C-9. The rate of flow is also less. The tank could not be emptied by gravity below point D.
Figure C-11. Uphill flow
SIZE OF PIPE
Figure C-12, shows a situation in which size of the line is increased at point X. Pressure lost because of friction is greater in smaller pipe than in the larger pipe. Therefore, the hydraulic gradient is not a straight line from A to B. Instead, it has a steeper slope from A to X and a lesser slope from X to B.
Figure C-12. Varying size of pipe
NEWSLETTER
|
Join the GlobalSecurity.org mailing list |
|
|