DHambley
Electrical
- Dec 7, 2006
- 246
As an electronics engineer I have limited knowledge of heat-flow equations and theory. However, on every new design I need to get a rough estimation of the thermal resistance of a metal to air boundary so I can at least know the temperature rise to within a 10C to 15C accuracy. This analysis will typically be done after the fact by a mechanical engineer or, by simply testing it after the design is mature. Hard to get a enclosure concept design going when the thermal picture is so vague.
Long ago a mechanical engineer gave me this equation for a the temperature rise of a cube in still, sea-level air: delT = (P * 1000 / area)^0.83 where P is in Watts and area is in cm^2. Another method I've used is finding curves of basic finned heat-sink shapes and interpolating from there. Seems a little crude but, that's all I've got to work with.
Do you have a set of ballpark or rule-of-thumb equations, especially at lower air density such as for aircraft, which you can share?
Thanks for your help.
Darrell Hambley P.E.
SENTEK Engineering, LLC
Long ago a mechanical engineer gave me this equation for a the temperature rise of a cube in still, sea-level air: delT = (P * 1000 / area)^0.83 where P is in Watts and area is in cm^2. Another method I've used is finding curves of basic finned heat-sink shapes and interpolating from there. Seems a little crude but, that's all I've got to work with.
Do you have a set of ballpark or rule-of-thumb equations, especially at lower air density such as for aircraft, which you can share?
Thanks for your help.
Darrell Hambley P.E.
SENTEK Engineering, LLC