Abstract

Sandwich panels are commonly used across industries for their ability to bear structural and thermal loads. In this paper, a panel chamber matching apparatus was designed to investigate the thermal performance of eight steel-based panels by exposing them to an impinging jet at approximately 550 °C for 30 min. Three types of low-cost materials (polycrystalline filaments, silica aerogel, and aluminum silicate) were used as the insulation core. The temperature of the panel surfaces was measured, as well as the metallic fasteners, including bolts, nails, battens, seams, and angle iron, to examine their thermal bridge effects. Major conclusions include the following: first, the maximum temperature on the impinged surface was consistent among all 20 cases, whereas that of the surface under free convection varied, ranging from 41 to 120 °C, depending on the core and thermal bridges. Second, most of the highest temperatures on opposite surfaces were caused by a section of bare angle iron, and this bridging effect could be significantly reduced by up to 50 °C using a few layers of cloth, although the improvement could be temporary. Bolts and nails were less effective as thermal bridges, while the battens could be more effective. Third, the estimated heat flux of all specimens ranged from 167 to 331 W·m−2.

Highlights

  • A sandwich panel, by definition, consists of a low-density core and one thin stiff layer bonded to each side [1,2]

  • A panel chamber matching setup was designed to investigate the thermal performance of sandwich panels under an impinging jet at 550 ◦ C for 30 min

  • Three types of low-cost materials that are commonly used in the shipbuilding industry were selected as the insulation core

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Summary

Introduction

A sandwich panel, by definition, consists of a low-density core and one thin stiff layer bonded to each side [1,2]. A sandwich panel with a metallic honeycomb core, a common example of PCM, is one of the most weight-efficient structures and can be extensively found in commercial aircraft [9,10,11,12]. In recent years, another group of PCMs, lattice structures, e.g., tetrahedral, pyramidal, Kagome, woven textile, and X-type lattices, have increasingly drawn attention, mostly owing to the open topology with embedded additional benefits [3,13,14,15,16,17]. For hypersonic aircraft, advanced sandwich panels using composite materials can be incorporated into the thermal protection system to protect the vehicle from overheating [20,21]

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