B Thermal Insulation Thickness Calculations

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The discussion centers on calculating insulation thickness using an online calculator that applies Fourier's law for heat conduction. Participants express curiosity about the equations behind the calculator, particularly regarding the inclusion of convection and radiation effects. One user is specifically calculating insulation for an engine bay with forced air cooling and seeks to understand the derivation of the thickness values provided by the calculator. They find discrepancies between their calculations and the calculator's output, prompting a request for advice on potential errors in their approach. The conversation highlights the complexity of heat transfer calculations and the importance of accurately determining parameters like the convection heat transfer coefficient.
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Derive equation used for insulation calculations.
I found this online calculator for insulation thickness: https://insulation.com.au/calculator/thickness-required/

Can you help me find equation being used for the calculation?

Based on inputs required, my understanding is that it must be heat conduction calculations but also accounting for convection and/or radiation effects on the inside and outside.

1711352992853.png
 
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:welcome: !

This calculator uses Fouriers law in one diimension. Familiar with that ?

Curiosity can be a reason to reverse-engineer that, but it may be more useful to build up your own calculation. What's your application ?

##\ ##
 
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I don't think that the calculator in your reference includes convective heat transfer resistance inside and outside the insulation.
 
Chestermiller said:
I don't think that the calculator in your reference includes convective heat transfer resistance inside and outside the insulation.

Change input to
1711365203329.png

and to
1711365247539.png

indicates it does, or am I mistaken ?

##\ ##
 
BvU said:
:welcome: !

This calculator uses Fouriers law in one diimension. Familiar with that ?

Curiosity can be a reason to reverse-engineer that, but it may be more useful to build up your own calculation. What's your application ?

##\ ##

I’m calculating insulation thickness for an engine bay with forced air cooling. Known parameters are
- inside air temperature (forced flow)
- outside air temperature (static)
- material properties of the engine bay enclosure and insulation, and finally
- maximum allowed outside surface temperature of the engine bay enclosure

The calculator I’ve given as an example is using all these as an input so this tells me I’m on the right track.

Ideally I’d like to plot the temperature on the outside of the engine bay enclosure vs insulation thickness

I could just use the calculator but I want to understand where the values are coming from just for my own curiosity :)

You mentioned Fouriers law which describes conductivity but this calculator seems to also account for convection. I’m not sure how to tackle that…
 
salvatore13 said:
I want to understand where the values are coming from just for my own curiosity :)
I can appreciate that !

Basically you have heat transfer ##\dot Q## over a series of resistances going from ##T_{hot} ## to ##T_{cold}##.

As with conductance, there is a relationship ##\dot Q = h A \Delta T## where all the knowledge is in the convection heat transfer coefficient ##h## ( W/(m2##\cdot##K) ).
##\Delta T## is the temperature difference between surface and bulk.

Ominously, my thermodynamics book (Cengel) says ##h## is an experimentally determined parameter whose value depends on all the variables that ... etc. Typical is 25-250 W/(m2##\cdot##K for forced convection of gases. Hmm...

(your calculator uses ##h = 22## it seems: 146 degrees with 'Inside surface temp equals operating temp' gives the same 22.48 mm).

##\ ##
 
BvU said:
I can appreciate that !

Basically you have heat transfer ##\dot Q## over a series of resistances going from ##T_{hot} ## to ##T_{cold}##.

As with conductance, there is a relationship ##\dot Q = h A \Delta T## where all the knowledge is in the convection heat transfer coefficient ##h## ( W/(m2##\cdot##K) ).
##\Delta T## is the temperature difference between surface and bulk.

Ominously, my thermodynamics book (Cengel) says ##h## is an experimentally determined parameter whose value depends on all the variables that ... etc. Typical is 25-250 W/(m2##\cdot##K for forced convection of gases. Hmm...

(your calculator uses ##h = 22## it seems: 146 degrees with 'Inside surface temp equals operating temp' gives the same 22.48 mm).

##\ ##
Thanks for the tip - I've tried to solve the problem and my equations give me somewhat sensible results but they don't match the result from the calculator. I'll try to walk you through it briefly.

The diagram for the problem:
1711449441450.png


For thermal equilibrium, I'm assuming that heat flux in and outside the panel must be equal so that temperatures remain constant.
##\dot Q_1 = \dot Q_2 = \dot Q_3## because ##T_1,T_2, T_{outside}, T_{inside} = constant##

For the worst-case scenario, ##\dot Q_1## can be omitted and simply
##T_1 = T_{inside}##

For Conduction through the insulation (##\dot Q_2##):
##\frac {\dot Q_2}{A} = \frac {T_1-T_2}{\frac {t_{ins}}{k_{ins}}}##
I'm ignoring the aluminium panel as it has a negligible thermal resistance.

For Convection between insulation and outside ambient air (##\dot Q_3##):
##\frac {\dot Q_3}{A} = h_3(T_2-T_{outside})##

So since:
##\dot Q_2 = \dot Q_3##

Then:
##\frac {T_1-T_2}{\frac {t_{ins}}{k_{ins}}} = h_3(T_2-T_{outside})##

And from that I come up with this solution for thickness:
##t_{ins} = \frac {k_{ins}(T_1-T_2)}{h_3(T_2-T_{out})}##

But when I plug in the same input from the calculator and h = 22, the result is thickness = 8.5mm instead 22.48 as it should be.

Any advice on what I'm doing wrong? :)
 
Last edited:
Let ##T_3## be the temperature between the aluminum and the insulation. Then, $$T_{outside}-T_1=\frac{q}{h_{outside}}$$
$$T_1-T_3=q\frac{b_{insulation}}{k_{insulation}}$$$$T_3-T_2=q\frac{b_{aluminum}}{k_{aluminum}}$$$$T_2-T_{inside}=\frac{q}{h_{inside}}$$. Add these equations together to eliminate T1, T2, and T3
 
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