Accidental Release Source Terms

Accidental release source terms are the mathematical equations that quantify the flow rate at which accidental releases of liquid or gaseous pollutants into the ambient environment can occur at industrial facilities such as petroleum refineries, petrochemical plants, natural gas processing plants, oil and gas transportation pipelines, chemical plants, and many other industrial activities. Governmental regulations in many countries require that the probability of such accidental releases be analyzed and their quantitative impact upon the environment and human health be determined so that mitigating steps can be planned and implemented.

There are a number of mathematical calculation methods for determining the flow rate at which gaseous and liquid pollutants might be released from various types of accidents. Such calculational methods are referred to as ''source terms'', and this article on accidental release source terms explains some of the calculation methods used for determining the mass flow rate at which gaseous pollutants may be accidentally released.

Accidental release of pressurized gas

When gas stored under pressure in a closed vessel is discharged to the atmosphere through a hole or other opening, the gas velocity through that opening may be choked (i.e., it has attained a maximum) or it may be non-choked.

Choked velocity, also referred to as sonic velocity, occurs when the ratio of the absolute source pressure to the absolute downstream pressure is equal to or greater than ''k'' + 1) / 2sup>''k'' / (''k'' − 1), where ''k'' is the specific heat ratio of the discharged gas (sometimes called the isentropic expansion factor and sometimes denoted as $\gamma$).

For many gases, ''k'' ranges from about 1.09 to about 1.41, and therefore ''k'' + 1) / 2sup>''k'' / (''k'' − 1 ) ranges from 1.7 to about 1.9, which means that choked velocity usually occurs when the absolute source vessel pressure is at least 1.7 to 1.9 times as high as the absolute downstream ambient atmospheric pressure.

When the gas velocity is choked, the equation for the mass flow rate in SI metric units is:''Perry's Chemical Engineers' Handbook'', Sixth Edition, McGraw-Hill Co., 1984.''Handbook of Chemical Hazard Analysis Procedures'', Appendix B, Federal Emergency Management Agency, U.S. Dept. of Transportation, and U.S. Environmental Protection Agency, 1989. Also provides the references below:
– Clewell, H.J., ''A Simple Method For Estimating the Source Strength Of Spills Of Toxic Liquids'', Energy Systems Laboratory, ESL-TR-83-03, 1983.
– Ille, G. and Springer, C., ''The Evaporation And Dispersion Of Hydrazine Propellants From Ground Spill'', Environmental Engineering Development Office, CEEDO 712-78-30, 1978.
– Kahler, J.P., Curry, R.C. and Kandler, R.A.,''Calculating Toxic Corridors'' Air Force Weather Service, AWS TR-80/003, 1980. Handbook of Chemical Hazard Analysis, Appendix B
Scroll down to page 391 of 520 PDF pages."Risk Management Program Guidance For Offsite Consequence Analysis"
U.S. EPA publication EPA-550-B-99-009, April 1999. (See derivations of equations D-1 and D-7 in Appendix D)"Methods For The Calculation Of Physical Effects Due To Releases Of Hazardous Substances (Liquids and Gases)", PGS2 CPR 14E, Chapter 2, The Netherlands Organization Of Applied Scientific Research, The Hague, 2005

: $Q \;=\; C\;A\; \sqrt$

or this equivalent form:

: $Q \;=\; C\;A\;P\;\sqrt$

For the above equations, it is important to note that although the gas velocity reaches a maximum and becomes choked, the mass flow rate is not choked. The mass flow rate can still be increased if the source pressure is increased.

Whenever the ratio of the absolute source pressure to the absolute downstream ambient pressure is less than
(''k'' + 1) / 2sup>''k'' / (''k'' − 1), then the gas velocity is non-choked (i.e., sub-sonic) and the equation for mass flow rate is:

: $Q \;=\; C\;A\;\sqrt$

or this equivalent form:

: $Q \;=\; C\;A\;P\; \sqrt$

The above equations calculate the initial instantaneous mass flow rate for the pressure and temperature existing in the source vessel when a release first occurs. The initial instantaneous flow rate from a leak in a pressurized gas system or vessel is much higher than the average flow rate during the overall release period because the pressure and flow rate decrease with time as the system or vessel empties. Calculating the flow rate versus time since the initiation of the leak is much more complicated, but more accurate. Two equivalent methods for performing such calculations are presented and compared at.

The technical literature can be very confusing because many authors fail to explain whether they are using the universal gas law constant ''R'' which applies to any ideal gas or whether they are using the gas law constant ''R''_s which only applies to a specific individual gas. The relationship between the two constants is ''R''_s = ''R''/''M''.

Notes:
* The above equations are for a real gas.
* For an ideal gas, ''Z'' = 1 and ''ρ'' is the ideal gas density.
* 1kilomole (kmol) = 1000moles = 1000 gram-moles = kilogram-mole.

Ramskill's equation for non-choked mass flow

P.K. Ramskill's equation for the non-choked flow of an ideal gas is shown below as equation (1):

: (1)       $Q = C \;\rho_A\;A\;\sqrt$

The gas density, ''$\rho$_A'', in Ramskill's equation is the ideal gas density at the downstream conditions of temperature and pressure and it is defined in equation (2) using the ideal gas law:

: (2)       $\rho_A = \frac$

Since the downstream temperature ''T_A'' is not known, the isentropic expansion equation below Isentropic Compression or Expansion
/ref> is used to determine ''T_A'' in terms of the known upstream temperature ''T'':

: (3)       $\frac = \left(\frac\right)^\frac$

Combining equations (2) and (3) results in equation (4) which defines ''$\rho$_A'' in terms of the known upstream temperature ''T'':

: (4)       $\rho_A = \frac$

Using equation (4) with Ramskill's equation (1) to determine non-choked mass flow rates for ideal gases gives identical results to the results obtained using the non-choked flow equation presented in the previous section above.

Evaporation of non-boiling liquid pool

Three different methods of calculating the rate of evaporation from a non-boiling liquid pool are presented in this section. The results obtained by the three methods are somewhat different.

The U.S. Air Force method

The following equations are for predicting the rate at which liquid evaporates from the surface of a pool of liquid which is at or near the ambient temperature. The equations were derived from field tests performed by the U.S. Air Force with pools of liquid hydrazine.

: $E = \left(4.161 \times 10^\right) \cdot u^ \cdot T_F \cdot M \cdot \frac$

If ''T''_P = 0°C or less, then ''T''_F = 1.0

If ''T''_P > 0°C, then ''T''_F = 1.0 + 0.0043 ''T''_P²

: $P_H = 760 \cdot e^$

The U.S. EPA method

The following equations are for predicting the rate at which liquid evaporates from the surface of a pool of liquid which is at or near the ambient temperature. The equations were developed by the United States Environmental Protection Agency using units which were a mixture of metric usage and United States usage. The non-metric units have been converted to metric units for this presentation.

: $E = \frac$

NB, the constant used here is 0.284 from the mixed unit formula/2.205lb/kg. The 82.05 become 1.0 = (ft/m)² × mmHg/kPa.

The U.S. EPA also defined the pool depth as 0.01m (i.e., 1cm) so that the surface area of the pool liquid could be calculated as:

:''A'' = (pool volume, in m³)/(0.01)

Notes:
* 1kPa = 0.0102kgf/cm² = 0.01bar
* mol = mole
* atm = atmosphere

Stiver and Mackay's method

The following equations are for predicting the rate at which liquid evaporates from the surface of a pool of liquid which is at or near the ambient temperature. The equations were developed by Warren Stiver and Dennis Mackay of the Chemical Engineering Department at the University of Toronto.Stiver, W. and Mackay, D., ''A Spill Hazard Ranking System For Chemicals'', Environment Canada First Technical Spills Seminar, Toronto, Canada, 1993.

: $E = \frac$

Evaporation of boiling cold liquid pool

The following equation is for predicting the rate at which liquid evaporates from the surface of a pool of cold liquid (i.e., at a liquid temperature of about 0°C or less).

: $E = 0.0001\;M (7.7026 - 0.0288\;B)\; e^$

Adiabatic flash of liquefied gas release

Liquefied gases such as ammonia or chlorine are often stored in cylinders or vessels at ambient temperatures and pressures well above atmospheric pressure. When such a liquefied gas is released into the ambient atmosphere, the resultant reduction of pressure causes some of the liquefied gas to vaporize immediately. This is known as "adiabatic flashing" and the following equation, derived from a simple heat balance, is used to predict how much of the liquefied gas is vaporized.

: $X = 100\;\frac$

If the enthalpy data required for the above equation is unavailable, then the following equation may be used.

: $X = 100 \cdot c_p \cdot \frac$

See also

*Choked flow
*Orifice plate
*Flash evaporation

References

{{reflist

External links

Ramskill's equations
are presented and cited in this pdf file (use search function to find "Ramskill").
Choked flow of gasesDevelopment of source emission models

Atmospheric dispersion modeling
Air pollution