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/(m
2##\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/(m
2##\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:
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? :)