STEP HEATING METHOD FOR THERMAL DIFFUSIVITY MEASUREMENT

Libor Vozár* and Tatiana Šrámková
*Department of Physics, Constantine the Philosopher University, Nitra, Slovakia
Institute of Physics, Slovak Academy of Sciences, Bratislava, Slovakia

Abstract: The paper presents the principle and mathematical basis of the step heating method for thermal diffusivity measurement. Here the known data reduction methods - procedures for analyzing the experimental temperature vs. time data, are summarized. The simple experimental apparatus is described and experimental results are given. The modification of the step heating method - the radial heat flow step heating technique, suitable for simultaneous measurement the axial thermal diffusivity (perpendicular to the plane faces of the sample) and radial thermal diffusivity (parallel to the plane faces), is described and discussed.

Keywords: thermal, diffusivity, step heating method

1 INTRODUCTION

The step heating method is an experimentally simple transient photothermal technique for the measurement of thermal diffusivity of solids. In this method the front face of a small thermally insulated disk-shaped sample is subjected to a constant heat flux condition. The resulting temperature rise of the rear face of the sample is recorded and the value of thermal diffusivity is computed from this temperature rise vs. time data [1-3].

The step heating method is an alternative technique to the well-known laser flash method, based on measurement and analyzing the temperature response at the rear face after the application of an instantaneous heat pulse on its front face [4]. Although the flash method has became the standard test technique, extensions of its use for some types of insulators, explosive and translucent materials is limited due to the relatively large temperature rise of the exposed front face. There are also difficulties involved in measuring the thermal diffusivity of large-grained heterogeneous materials, especially oriented fiber-reinforced composites, where the scale of microstructure is usually comparable with the used sample thickness. Substituting step heating for laser pulse tends to overcome these difficulties. The possibility to use samples of relatively large dimensions in comparison to those used in the flash method allows to extend cases, where the material can be considered to behave as a homogeneous medium. Another advantage of the step heating method is relatively low intensity of the imposed heat flux in comparison with that necessary for the pulse heating techniques. The sample is thereby less likely to exhibit a phase transition or decompose as a result of a sudden large temperature increase at the front face.

2 MATHEMATICAL BASIS

The ideal model of the step heating method is based on the behavior of a homogeneous, thermally insulated, infinite slab, with uniform and constant thermal properties and density, initially at constant (zero) temperature, subjected to a constant heat flux, uniformly applied since the time origin (t=0), over its front face (x=0). The transient temperature T(x,t)=T(e,t) of the rear face of the sample can be received in the form [1-3]
.
(1)
Here a is the thermal diffusivity, r the density, c the specific heat and q is the heat flux supplied to the unit area of the front face. Use of the simple adiabatic model is limited due to the difficulty of creating the ideal conditions considered as initial and boundary conditions in the mathematical model. In a real experiment heat transfer between the sample and its environment is often unavoidable, especially at high temperatures and/or by measurement of poor conductive materials.

The non-ideal model considers a disk-shaped sample with radius rs and takes into account linearized heat losses from the sample governed by Biot numbers related to front, rear and lateral faces (H0, He and Hr ) [3]. The temperature T(x,r,t)=T(e,0,t) in the center of rear face can be written as
Eq 2.,
(2)
where An, Bm, un, and wm are variables defined in appendix.

3 DATA REDUCTION

An estimation of thermal diffusivity can be performed by comparing the experimental data and temperature rise vs. time curves computed from an appropriated model. This is possible by calculation and comparing of ratio V of temperatures V=T(t1)/T(t2) in various times t1 and t2 as proposed in [1,2].

More efficient are parameter estimation techniques, based on a least squares fitting. Conditions for successful application of a least-squares fitting in data analysis result from sensitivity analysis, performed by calculating normalized sensitivity coefficients, defined as
Eq 3..
(3)
Here b is the appropriated fit parameter and T is the temperature. When taking the ideal adiabatic model (1), results show that sensitivity for thermal diffusivity a and sensitivity for heat flux term B=q/rce vs. time curves are linearly independent (figure 1). That means that the necessary condition for least squares fitting is fulfilled and an unique estimation of parameters a and B is possible [5]. Figure 2 shows results of sensitivity analysis performed considering the model with heat losses from the axial (front, rear) and lateral faces (Ha=H0=He). We see, that sensitivities for axial and radial Biot numbers are close to being linearly dependent. This indicates, that the simultaneous estimation of parameters Ha and Hr may be difficult, therefore it is suitable to assume that there are equal axial and radial heat transfer coefficients and axial and radial Biot numbers fulfill the condition
Eq 4..
(4)

Fig 1. Sensitivity coefficient curves for the adiabatic model
Figure 1. Sensitivity coefficient curves for the adiabatic model (1) (a=5.10-5 m2.s-1; B=1 K.s-1; e=10 mm).
Fig 5. Sensitivity coefficient curves for the model with heat losses
Figure 2. Sensitivity coefficient curves for the model with heat losses (2) (a=5.10-5 m2.s-1; B=1 K.s-1; H0=He=0,1; Hr=0,05; e=10 mm; rs=5 mm).

Thus data reduction consists of searching of three unknown parameters a, B and Ha which unique estimation is possible. The paper [3] detailed describes application of the ordinary least squares (OLS) and the Levenberg-Marquardt (LM) fitting methods in the data reduction process.

Another way is to utilize the Fourier transformation for transformation of the experimental data and then to fit the image temperature with a proper formula [6]. The main advantage of the method is in insensitivity of the thermal diffusivity calculation on the temperature level before the step heating application (base line) and in independency of results on the disturbing of the data by a linearly rising or falling signal.

4 EXPERIMENTAL APPARATUS

The step heating apparatus built in the Thermophysical Laboratory in Nitra consists of the heat source, a halogen lamp (12V/100W) with a parabolic reflector, and the electrically controlled mechanical light shutter. The lamp is powered by a direct current produced by stabilized current/voltage supply Z-YE-2T-X (Mesit) with the unit of remote control JDR-1 (Mesit). The setting of optimal current depends on sample thermal properties and dimensions and is chosen so the rear face temperature rise reaches about 1-3°C in the measurement. The measurement time is taken from optimal experimental design analysis (tn+=a.tn/e2 ~ 5 when taking equation (2)[7]). The temperature rise at the rear face is measured by spot welded K-type thermocouple (NiCr/Ni wires (Heraeus) 0,1 mm in diameter). The reference cold junction is immersed in Dewar cup at 0°C. The transient emf of the thermocouple is amplified and digitized by standard 12-bit A/D converter. The apparatus is fully controlled by a PC.

For this apparatus a software package was written, which allows device control, data acquisition and data analysis. The measurement cycle starts with continuous measurement of rear face temperature vs. time evolution. When a thermal equilibrium in the sample fixes, the data acquisition task performs the data acquisition. When executed, it first switches on the halogen lamp, and then the routine reads the transient voltage from the temperature sensor. When the heat flowing from the lamp is stabilized and after the time equal to 10% of the total measurement time the light shutter puts on and the step (continuous) heating starts. The data acquisition rate is controlled with the use of a quartz time base and 8253 counter. The data reduction consists in performing least squares fits of the measured temperature vs. time data as described in part 3. Then the data are analyzed, the received results are printed and/or saved, and the described measurement cycle starts again. That allows the measurement to be conducted in a fully automatic way.

In order to demonstrate that the instrument operates in accordance with the appropriated mathematical model, a number of measurement are performed. Figure 3 presents typical

Fig 3. Experimental rear face temperature vs. time curves
Figure 3. Experimental rear face temperature vs. time curves (graphite e=27 mm; steel e=6 mm).

rear face temperature rise vs. time vs. time evolution obtained measuring graphite and stainless steel samples at room temperatures. The received values of thermal diffusivity gained using the OLS and LM together with the values given by NIST [8,9] are given in the table 1.

Table 1. Thermal diffusivity of graphite and stainless steel calculated using OLS and LM fitting method compared with recommended literature values.
Table 1.

5 RADIAL HEAT FLOW STEP HEATING METHOD

Although the step heating method was originally designed for the measurement of the thermal diffusivity of isotropic solids, the possibility of its use for measurement of anisotropic material has been shown [10]. The radial heat flow step heating method consists in irradiating the central circular area of radius smaller than the sample radius. If the temperature response is measured at rear face the axial thermal diffusivity (perpendicular to the plane faces of the sample) as well as radial thermal diffusivity (parallel to the plane faces) can be deduced from these temperature rise vs. time curves.

Let us consider a cylindrical sample of radius rs and thickness e subjected to a constant heat flux per unit surface q, uniformly applied since the time origin over a central circular area of radius rp smaller than sample radius rs (figure 4). This presents a symmetry around the principal

Fig 4. Mathematical model of the radial heat flow step heating method
Figure 4. Mathematical model of the radial heat flow step heating method.

axis x and it is easy to show, that the transient temperature T=T(x,r,t) in position (x,r) of the sample can be expressed by formula
Eq 5.,
(5)
where aa is the axial and ar the radial thermal diffusivity. It was shown, that the temperature evolution measured at rear face may contain enough information for a unique estimation of both diffusivities [10].

The measurement of a temperature rise response curves in several different positions on rear face increases the precision of the radial thermal diffusivity estimation, which is in general strongly dependent on the knowledge of exact detector position, difficult to measure precisely. The use of repeated measurements results not only in decreasing statistical errors, but also in minimizing the influence of many experimental errors, like calibration errors of temperature sensors, local sample material non-homogenities, uncertainties in knowing temperature sensor locations, etc.

Sensitivity analysis shows that the data reduction - estimation parameters aa, ar, B and H, based on a least squares fitting can be succesfully applied for unique estimation of all parameters. The data reduction can be viewed as an explicit multiresponse ordinary least squares problem for multivariate explanatory data. Results of Monte Carlo simulations and simulated data analysis confirm, that both - axial and radial thermal diffusivity can be estimated with the similar accuracy [10].

APPENDIX

, H0 > 0; He > 0

, Hr > 0

where un and wm are the positive roots of equations

,

and J0 and J1 are Bessel functions of the first kind, order 0 and 1.

REFERENCES

[1] R.R. Bittle, R.E. Taylor, Step-heating technique for thermal diffusivity measurements of large-grained heterogeneous materials, J. Amer. Ceram. Soc. 67 (1984) 186-190.
[2] R.R. Bittle, R.E. Taylor, Thermal diffusivity of heterogeneous materials and non-fibrous insulators, in T. Ashword , D.R. Smith (ed.), Thermal Conductivity, Vol. 18, Plenum, New York, 1985, p. 379-390.
[3] L. Vozár, T. Šrámková, Two data reduction methods for evaluation of thermal diffusivity from step heating measurements, Int. J. Heat Mass Transfer (in press)
[4] W.J. Parker, R.J. Jenkins, C.P. Butler, G.L. Abbott, Flash method of determining thermal diffusivity, heat capacity and thermal conductivity, J. Appl. Phys. 32 (1961) 1679-1684.
[5] J.V. Beck, K.J. Arnold, Parameter Estimation in Engineering and Science, John Wiley and Sons, New York, 1977, 349 p.
[6] J. Gembaroviè, R.E. Taylor, Using the cosine Fourier transform in thermal diffusivity measurement, High Temp. High Press (accepted).
[7] L. Vozár, G. Groboth, Thermal diffusivity measurement of poor conductive materials. A comparison of step heating to flash method, High Temp. High Press (accepted).
[8] J.G. Hust, A.B. Lankford, A fine-grained, isotropic graphite for use as NBS thermophysical property RM's from 5 to 2500 K. National Bureau of Standards, 1984, p. 260-289.
[9] J.G. Hust, A.B. Lankford, Austenitic stainless steel thermal conductivity and electrical resistivity as a function of temperature from 5 to 2500 K. National Bureau of Standards, Certificate Standard Reference Materials 1460, 1461, 1462, Washington DC, 1984.
[10] L. Vozár, T. Šrámková, Simultaneous measurement of axial and radial thermal diffusivities of anisotropic media using the radial heat flow step heating method, High Temp. High Press. (accepted).

Contact point: Libor Vozár, Department of Physics, Faculty of Natural Sciences, Constantine the Philosopher University, Tr. A. Hlinku 1, SK-94974 Nitra, Slovakia, Phone + 42 87 511073, Fax + 42 87 511243, E-mail: lvozar@ukf.sk