zmis
Chemical
- Mar 26, 2010
- 4
I'm trying to verify the temperature of a stack's steel (A36) structure.
8.33' OD, 2" of concrete insulation on the inside for an 8.0' ID.
I know the bulk fg temperature (529F), the ambient temperature (105F), thermal conductivity of the insulation (1.54 Btu*in/ft2*hr*F or 0.1283 Btu/ft*hr*F) and gas flow characteristics (163167 lb/hr @ 23.1 ft/s).
I've referenced ASME STS-1 and my old transport text. STS-1 indicates a free convection external heat transfer coefficient of about 1 to 1.1 (fig B2-1) and an internal heat transfer coefficient of about 2.7 (fig B1). I'm ignoring the contribution of the 1/4" A36 shell (k~24 btu/ft*hr*F).
I keep thinking this should be simple now, but it's not coming to me. I've set the three q values (internal film, conduction in the insulation, external film) to approximately equal by varying the hot and cold face temperatures of the concrete and stack shell. This gives me a q value and cold face temperature significantly different than the lightweight program we use to set refractory thickness (provided by the refractory manufacturers). I've tried tossing in radiative losses (and they *should* be in there at some point) but that gets me very far off once the 0.95 emissivity in the program is plugged in. If I use about 0.4 for the painted surface I get a lot closer but I'm still not certain I'm doing this right.
Isn't there a simpler calculation for the cold face temperature? STS-1 doesn't call it out explicitly and all of the formulae that are listed would require it to be a function of itself (which is what I'm doing iterating wall temperature changes until the q's are equal). Any suggestions? I really don't mind feeling like an idiot at this point, as I've got an expiditer hounding me for this documentation, so please feel free to tell me to "look it up" etc, just do so while pointing towards the solution please. (i.e. "look it up on page xx of spec API-yyy)
Thanks in advance.
8.33' OD, 2" of concrete insulation on the inside for an 8.0' ID.
I know the bulk fg temperature (529F), the ambient temperature (105F), thermal conductivity of the insulation (1.54 Btu*in/ft2*hr*F or 0.1283 Btu/ft*hr*F) and gas flow characteristics (163167 lb/hr @ 23.1 ft/s).
I've referenced ASME STS-1 and my old transport text. STS-1 indicates a free convection external heat transfer coefficient of about 1 to 1.1 (fig B2-1) and an internal heat transfer coefficient of about 2.7 (fig B1). I'm ignoring the contribution of the 1/4" A36 shell (k~24 btu/ft*hr*F).
I keep thinking this should be simple now, but it's not coming to me. I've set the three q values (internal film, conduction in the insulation, external film) to approximately equal by varying the hot and cold face temperatures of the concrete and stack shell. This gives me a q value and cold face temperature significantly different than the lightweight program we use to set refractory thickness (provided by the refractory manufacturers). I've tried tossing in radiative losses (and they *should* be in there at some point) but that gets me very far off once the 0.95 emissivity in the program is plugged in. If I use about 0.4 for the painted surface I get a lot closer but I'm still not certain I'm doing this right.
Isn't there a simpler calculation for the cold face temperature? STS-1 doesn't call it out explicitly and all of the formulae that are listed would require it to be a function of itself (which is what I'm doing iterating wall temperature changes until the q's are equal). Any suggestions? I really don't mind feeling like an idiot at this point, as I've got an expiditer hounding me for this documentation, so please feel free to tell me to "look it up" etc, just do so while pointing towards the solution please. (i.e. "look it up on page xx of spec API-yyy)
Thanks in advance.