In previous post, i have informed the first errata in API Std 521, edition Jan 2007. As expected more reading on this code found another discrepancy compare to previous version. This discrepancy is mainly due to REMOVAL of specific heat ratio (k) in the Mach number and Critical pressure calculation.
Equation [23] & [24] and [25] & [26] in API RP 521, 1997 (previous revision) are used to calculate the Mach number and Critical pressure of gas in the pipe.
Mach number
In imperial unit,
In metric unit,
Critical pressure
In imperial unit,
In metric unit,
After the API RP 521 is updated, similar equations used to calculate Mach number and Critical pressure has minimum modification.
Mach number
In imperial unit,
In metric unit,
Critical pressure
In imperial unit,
In metric unit,
Detail review on above equations, the specific heat capacity ratio (k) has been removed from the original equation. Is this a correction or an error ?
I have made some literature surveys and conduct some derivation works. Two main findings :
Based on simple derivation works, it ended-up with inclusion of k factor in the equation.
This discrepancy has been highlighted to API committee manager attention and quick response indicated equations in current edition (2007) are correct where k factor should not appear in those equations. Due to manning issue, no detail basis disclosed. Details searching do not find any supporting documents.
k factor generally range from 1.09 to 1.41 for most gases. Inverse square-root of k would range from0.84 to 0.96. Inclusion of k in the equation would probably bring down Mach number and critical pressure. Both impacts are partially balancing each and minimum impact to flowrate.
After further discussion and anaylsis, it's found that considering isothermal flow, the k factor should be omitted from the Mach number and critical pressure calculation. Details derivation may refer to "Removal of Specific Heat ratio (k) in the Mach No. & Critical Pressure Calculation".
Updated
- Nov 8, 2007 : This issue is being discussed in CheResource forum (Click HERE to view)
- Sept 28, 2008 : Post updated with omission of k factor.
- API R 521 1993 – No specific heat capacity ratio (k) included in the equation. However, API has included the k factor into the equation when it revised to API RP 1997. Once again, when it revised recently to 2007, the k factor has been removed again.
- Quick derivation showed that k factor should appear in the equation.
Based on simple derivation works, it ended-up with inclusion of k factor in the equation.
This discrepancy has been highlighted to API committee manager attention and quick response indicated equations in current edition (2007) are correct where k factor should not appear in those equations. Due to manning issue, no detail basis disclosed. Details searching do not find any supporting documents.
k factor generally range from 1.09 to 1.41 for most gases. Inverse square-root of k would range from0.84 to 0.96. Inclusion of k in the equation would probably bring down Mach number and critical pressure. Both impacts are partially balancing each and minimum impact to flowrate.
After further discussion and anaylsis, it's found that considering isothermal flow, the k factor should be omitted from the Mach number and critical pressure calculation. Details derivation may refer to "Removal of Specific Heat ratio (k) in the Mach No. & Critical Pressure Calculation".
Updated
- Nov 8, 2007 : This issue is being discussed in CheResource forum (Click HERE to view)
- Sept 28, 2008 : Post updated with omission of k factor.
Further Reading :
- Removal of Specific Heat ratio (k) in the Mach No. & Critical Pressure Calculation
- Controlled and Non-controlled Type Depressuring.
- How to apply valve equation in HYSYS Depressuring ?
- 12 Features required for Shutdown Valve (SDV)
- ERRATA - API Std 521, Pressure Relieving and Depressuring Systems
- Requirement of overpressure protection devices on system design to PIPING code
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