Abstract
The heat-transfer behaviour of the conduction cold plate system used for avionics is investigated in this paper. The steady-state temperature profile for the cold plate is derived and the relationship between the coolant mass flowrate, the heat load and the highest cold plate temperature is established. A model is proposed to describe the transient thermal rosponse of the cold plate under thermal shock condition. The analytic solution of the transient heat transfer within the cold plate is provided. The results of this paper agree with those of the finite element method and can be used for the structural design and performance evaluation of cold plate system.
| Original language | English |
|---|---|
| Pages (from-to) | 236-240 |
| Number of pages | 5 |
| Journal | Journal of Thermal Science |
| Volume | 4 |
| Issue number | 4 |
| DOIs | |
| State | Published - Oct 1995 |
Keywords
- avionics
- cold plate
- conduction cooling system
- heat transfer
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