anousone
Civil/Environmental
- Aug 8, 2003
- 5
Hi,
I need to design venting area for a gas deflagration in an empty tank (no obstacles).
As specified in the NFPA 68, the Kg values are dependent on the volume of the vessel. If I used the Kg value corresponding to my volume (read from the figure Kg vs volume) the required venting area calculated is too high for practical purpose. And I didn't even consider initial turbulence and potential inertia effects...
Does anyone know about papers or articles that have dealt with the Kg variation with wolume or that have shown that it is acceptable to use the Kg values measured in the 5L sphere?
Thanks.
I need to design venting area for a gas deflagration in an empty tank (no obstacles).
As specified in the NFPA 68, the Kg values are dependent on the volume of the vessel. If I used the Kg value corresponding to my volume (read from the figure Kg vs volume) the required venting area calculated is too high for practical purpose. And I didn't even consider initial turbulence and potential inertia effects...
Does anyone know about papers or articles that have dealt with the Kg variation with wolume or that have shown that it is acceptable to use the Kg values measured in the 5L sphere?
Thanks.