Gas-release.
xlsm
Instruction: This spreadsheet computes gas volume release based on black oil model calculation
Instruction: 1) SUpdate data in the Input Data section; 2) Click Solution button; 3) View result.
Input Data: 1
Input data Results
Components Lobitos Mwa MWg 20.1345
N2 0.4679 28.01 SG 0.6967
CO2 0.215 44.01 Tpc 388 °R
H2S 0 98.08 Ppc 669 psia
C1 85.7368 16.04 Top 110.0 °F 570.0 °R
C2 6.1766 30.07 Pop 900.0 psia
C3 3.5415 44.10 Ppr 1.34
iC4 1.327 58.12 Tpr 1.47
nC4 1.3965 58.12 Zf 0.876053577
iC5 0.5909 72.15 Zi
nC5 0.3454 72.15 Slope -0.092
nc6 0.2358 86.18 Cpr 0.848817363
nc7 0.1756 100.20 Cg* 0.001268314
nc8 0.0853 114.23 Cg 0.0011111111
C6+ 47/35/17 0.4966 - L 23 ft
D 1.94 in
Temperature i 110 °F V 0.4636 ft3
Temperature f 60 °F V 22.6831 scf
Pressure i 900 psia ΔV/ΔP 0.02520 ft3/psi
Pressure f 14.7 psia ΔP 885.3 *900 a 14.7 psig
ΔV 22.3127
Total 44.9958 scf
Hall-Yarborogh-z.xlsm
Instruction: This spreadsheet computes gas compressibility factor with Hall-Yarborough method.
Instruction: 1) Select a unit system; 2) Update data in the Input Data section; 3) Click Solution button; 4) View result.
Input Data: 1
Temperature: 110 oF 100
Pressure: 900 psia 1
Gas specific gravity: 0.70 air = 1 0.7
Nitrogen mole fracytion: 0 0.05
Carbon dioxide fraction: 0 0.05
Hydrogen sulfite fraction: 0 0.02
T pc 326 315.7( g 0.5) 83.3 y CO2
240Ry N 2 370.86959091
= 388.09652536 o
p pc 678 50( g 0.5) 206 y N2
.7 psia
= 668.16526364 440 y CO2
4.5453419295
T
T pr = 1.5415347909
T pc
1
tr = 0.6487041395
T pr
p
p pr = 1.3469721474
p pc
)2
A 0.06125 tr e 1.2 (1 t r
= 0.034263984
B t r 14.76 9.76t=r6.7179734101
4.58t r
2
C tr 90.7 242.2t 42.4t r
= -31.50983001
r
2
D 2.18 2.82
= 4.0093456733
tr
Y = ASSUMED = 0.052682431
Y Y 2 Y 3 Y 4 = 0.0003632015
f (Y ) Ap pr BY 2
CY
(1 Y ) 3
= 0.876053577
Ap pr
z
Y
2 .7 p
= 3.3903401617 lbm/ft3 54.195472553
g
g
zT
C 570 oF
MPa 900 psia
air = 1 0.6966947271 air=1
0
0
0
83.K3 y CO2 133.3 y H s S
o
440
MPay
CO2 606.7 y H s S
58t r
2
.4t r
2
BY 2
CY D
0
kg/m3