Measurement of the In-plane Thermal Diffusivity and Temperature-Dependent Convection Coefficient Using a Transient Fin Model and Infrared Thermography

• Published in: International journal of thermophysics 2009-12, Vol.30 (6), p.1902-1917
• Main Authors: Miettinen, L., Kekäläinen, P., Merikoski, J., Timonen, J.
• Format: Article
• Language: English
• Subjects: Classical Mechanics; Coefficients; Condensed Matter Physics; Convective heat transfer; Fittings; Heat loss; Industrial Chemistry/Chemical Engineering; Mathematical models; Physical Chemistry; Physics; Physics and Astronomy; Temperature distribution; Thermal diffusivity; Thermography
• ISSN: 0195-928X; 1572-9567
• DOI: 10.1007/s10765-009-0690-3

The transient fin model introduced recently for determination of the in-plane thermal diffusivity of planar samples with the help of infrared thermography was modified so as to be applicable to poor heat conductors. The new model now includes a temperature-dependent heat loss by convective heat transfer, suitable for an experimental setup in which the sample is aligned parallel to a weak, forced air flow stabilizing otherwise the convective heat transfer. The temperature field in the sample was measured with an infrared camera while the sample was heated at one edge. The symmetric temperature field created was averaged over the central fifth of the sample to obtain one-dimensional temperature profiles, both transient and stationary, which were fitted by a numerical solution of the fin model. One of the fitting parameters was the thermal diffusivity, and with a known density and specific heat capacity, the thermal conductivity was thus determined. The test measurements with tantalum samples gave the result (57.5 ± 0.2) W · m −1 · K −1 in excellent agreement with the known value. The other fitting parameter was a temperature-dependent heat loss coefficient from which the lower limit for the temperature-dependent convection coefficient was determined. For the stationary state the result was (1.0 ± 0.2) W · m −2 · K −1 at the temperature of the flowing air, and its temperature dependence was found to be (0.22 ± 0.01) W ·m −2 · K −2 .