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July 5, 2013 17:13
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python: AGA3 GAS FLOW CALCULATION
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# -*- coding: utf-8 -*- | |
""" | |
Created on Fri Aug 27 09:16:20 2010 | |
@author: g.junqueira | |
AGA3 METER GAS CALCULATION IMPLEMENTATION as a callable Python function | |
""" | |
import math | |
def AGA3 (DP, Tf, Pf, DFLOW, Dr, ALPHA2,ALPHA1=0.00000925,Tr=60.0, Pb=14.73): | |
""" | |
Inputs: | |
DP = Differential pressure, in Inches H2O | |
Tf = Flowing Temperature Meter, in Deg. F. | |
Pf = Flowing Pressure meter, in psig | |
Tb = Base temprature, in Deg. F. (60 deg. F , as defined in USC) | |
Pb = Base pressure, in psia (14.73psia, as defined in USC) | |
Dr = reference orifice plate bore diameter at Tr, in inches | |
ALPHA1 = linear coefficient of thermal expansion for orifice plate material, in in/in-DegF | |
carbon steel (0.00000620), 304 or 316 stainless (0.00000925), | |
monel (0.00000795), Hastalloy C (0.0000063) | |
""" | |
return 0 | |
def __orifBore(Dr, Tf, ALPHA1=0.00000925, Tr=60.0): | |
""" | |
calculates orifice bore diameter at flowing conditions (d) | |
""" | |
d = Dr*(1.0 + ALPHA1*(Tf-Tr)) | |
return (d) | |
def __pipeIntDiam (Dr, ALPHA2, Tf, Tr=60.0): | |
""" | |
""" | |
D = Dr*(1.0 + ALPHA2*(Tf-Tr)) | |
return (D) | |
def __velOfApproach (d, D): | |
""" | |
""" | |
__Beta = d/D | |
__Beta2 = math.pow(__Beta, 4.0) | |
Ev = 1.0/(math.sqrt((1.0-__Beta2))) | |
return (Ev) | |
def __unitConversion (unit=0): | |
""" | |
0 = U.S | |
1 = IP | |
2 = Metric | |
3 = SI | |
""" | |
__const0 = 3.232790 * math.pow(10.0, 2.0) | |
__const1 = 4.655210 * math.pow(10.0, 4.0) | |
__const2 = 3.600 * math.pow(10.0,-2.0) | |
__const3 = 1.0 | |
if unit ==1: | |
N1 = __const1 | |
elif unit ==2: | |
N1 = __const2 | |
elif unit ==3: | |
N1 = __const3 | |
else: | |
N1 = __const0 | |
return (N1) | |
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It looks like this is pretty incomplete. Did you ever finish the calculations?