and L. V. Mial′We propose a method for determining the longitudinal thermal conductivity of thin-walled structural elements from composite materials involving the formation in the sample of the investigated material of a nonstationary temperature fi eld whose gradient coincides with the direction of the reinforcement plane. We have made estimates of the infl uence of the main methodological errors of the proposed method on the determination accuracy of the thermal conductivity of the material.
Introduction.Composite materials (CM) having a unique complex of mechanical, thermal, and electrophysical properties fi nd expanding applications in rocket-space technology. One promising fi eld of application of such materials is large-sized space structures that must possess high stiffness and strength at a minimum weight. The development of such structures from composite materials is a complicated interdisciplinary problem, in the solution of which the need arises for complete and reliable data on the thermal characteristics of the above materials. In thin-walled elements of large-sized space structures (panels, sheaths, bars, cables), the transverse temperature differences are not great, as a rule, and practically do not depend on their thermal conductivity in the direction perpendicular to the reinforcement plane. However, under inhomogeneous heating of such elements, an important role in the formation of their temperature fi elds is played by the socalled longitudinal thermal conductivity, i.e., the thermal conductivity in the reinforcement plane of the composite material. Unfortunately, the thermal conductivity of composite materials in the direction of their reinforcement is as yet imperfectly understood. An attempt to fi ll the gap in understanding this phenomenon was made in [1].At present, many methods for investigating the thermal conductivity of composite materials, of which the absolute stationary method [2] is considered to be classical, are used. In this method, a plane sample of thickness δ much smaller than its characteristic size l (l/δ ≥ 5) is placed between a heater and a cooler. To lower the lateral heat exchange of the sample, auxiliary guard heaters and effective heat-insulating materials are used. However, the absolute stationary method is not suitable for determining the thermal conductivity in the reinforcement plane of sheaths and bars made from composite materials, since the geometry of such elements excludes the possibility of creating samples satisfying the indicated restriction on the geometric sizes of the investigated sample.To investigate the thermal conductivity of composite materials, TPS methods based on the application of thermistors are also used [3]. In this case, the thermistor placed between two identical samples serves as both a heat source and a resistance thermometer. Such methods are based on the semibounded space theory and are applicable for investigating samples of suffi cient thickness, which is diffi cult for sheaths, bars, and cables.The thermal properties of a composite ...