## Accidental release source terms – wikipedia impact of electricity in the 1920s

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.

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) / 2] k / ( k − 1), where k is the specific heat ratio of the discharged gas (sometimes called the isentropic expansion factor and sometimes denoted as γ {\displaystyle \gamma } ).

For many gases, k ranges from about 1.09 to about 1.41, and therefore [( k + 1) / 2] 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: [1] [2] [3] [4] Q = C A k ρ P ( 2 k + 1 ) k + 1 k − 1 {\displaystyle Q\;=\;C\;A\;{\sqrt {\;k\;\rho \;P\;\left({\frac {2}{k+1}}\right)^{\frac {k+1}{k-1}}}}}

Whenever the ratio of the absolute source pressure to the absolute downstream ambient pressure is less than [ ( k + 1) / 2] 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 2 ρ P [ k k − 1 ] [ ( P A P ) 2 k − ( P A P ) k + 1 k ] {\displaystyle Q\;=\;C\;A\;{\sqrt {\;2\;\rho \;P\;\left[{\frac {k}{k-1}}\right]\left[\left({\frac {P_{A}}{P}}\right)^{\frac {2}{k}}-\;\,\left({\frac {\;P_{A}}{P}}\right)^{\frac {k+1}{k}}\;\right]}}}

or this equivalent form: Q = C A P [ 2 M Z R T ] [ k k − 1 ] [ ( P A P ) 2 k − ( P A P ) k + 1 k ] {\displaystyle Q\;=\;C\;A\;P\;{\sqrt {\left[{\frac {2\;M}{Z\;R\;T}}\right]\left[{\frac {k}{k-1}}\right]\left[\,\left({\frac {P_{A}}{P}}\right)^{\frac {2}{k}}-\;\,\left({\frac {P_{A}}{P}}\right)^{\frac {k+1}{k}}\;\right]}}} where:

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 www.air-dispersion.com/feature2.html.

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.

P.K. Ramskill’s equation [5] [6] for the non-choked flow of an ideal gas is shown below as equation (1): (1) Q = C ρ A A 2 P ρ ⋅ k k − 1 ⋅ [ 1 − ( P A P ) k − 1 k ] {\displaystyle Q=C\;\rho _{A}\;A\;{\sqrt {{\frac {\;\,2\;P}{\rho }}\cdot {\frac {k}{k-1}}\cdot \left[\;1-{\left({\frac {P_{A}}{P}}\right)^{\frac {k-1}{k}}}\right]}}}

The *gas density*, ρ {\displaystyle \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) ρ A = M P A R T A {\displaystyle \rho _{A}={\frac {M\;P_{A}}{R\;T_{A}}}}

Since the downstream temperature T A is not known, the isentropic expansion equation below [7] is used to determine T A in terms of the known upstream temperature T: (3) T A T = ( P A P ) k − 1 k {\displaystyle {\frac {T_{A}}{T}}=\left({\frac {P_{A}}{P}}\right)^{\frac {k-1}{k}}}

Combining equations (2) and (3) results in equation (4) which defines ρ {\displaystyle \rho } A in terms of the known upstream temperature T: (4) ρ A = M P k − 1 k R T P A − 1 k {\displaystyle \rho _{A}={\frac {M\;P^{\frac {k-1}{k}}}{R\;T\;P_{A}^{-{\frac {1}{k}}}}}}

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 [ edit ]

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. [2] E = ( 4.161 × 10 − 5 ) ⋅ u 0.75 ⋅ T F ⋅ M ⋅ P S P H {\displaystyle E=\left(4.161\times 10^{-5}\right)\cdot u^{0.75}\cdot T_{F}\cdot M\cdot {\frac {P_{S}}{P_{H}}}} where:

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. [3] The non-metric units have been converted to metric units for this presentation. E = 0.1288 ⋅ A ⋅ P ⋅ M 0.667 ⋅ u 0.78 T {\displaystyle E={\frac {0.1288\cdot A\cdot P\cdot M^{0.667}\cdot u^{0.78}}{T}}}

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. [8] E = k ⋅ P ⋅ M R ⋅ T A {\displaystyle E={\frac {k\cdot P\cdot M}{R\cdot T_{A}}}} where:

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). [2] E = 0.0001 M ( 7.7026 − 0.0288 B ) e − ( 0.0077 B ) − 0.1376 {\displaystyle E=0.0001\;M(7.7026-0.0288\;B)\;e^{-(0.0077\;B)-0.1376}} where:

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 H s L − H a L H a V − H a L {\displaystyle X=100\;{\frac {H_{s}^{L}-H_{a}^{L}}{H_{a}^{V}-H_{a}^{L}}}} where: