Scale modeling of thermo-structural fire tests of multi-orientation wood laminates

Abstract

The stacking sequence of laminated wood significantly impacts the composite mechanical behavior of the material, especially when scaling down thermo-mechanical tests on plywood. In previous research, we developed a scaling methodology for thermo-structural tests on samples with similar cross sections, however this paper focused on testing plywood samples with different stacking sequences between the scales. Plywood samples at 1/2 -scale and 1/4 -scale were subjected to combined bending and thermal loading, with the loading scaled to have the same initial static bending stresses. While the 1/4 -scale 4-layer [0 degrees/90 degrees]s laminate and the 1/2 -scale 8-layer [0 degrees/90 degrees/90 degrees/0 degrees]s laminate had an equal number of 0 degrees and 90 degrees layers, as the char front progresses, the sections behave differently. Thus, modeling becomes essential to extrapolating the data from the smaller 1/4 -scale test to predict the behavior of the larger 1/2 -scale test. Reduced cross-sectional area models (RCAM) incorporating classical laminated plate theory were used to predict the mechanical response of the composite samples as the char front increased. Three methods were proposed for calibrating the RCAM models: Fourier number scaling, from detailed kinetics-based pyrolysis GPyro models, and fitting to data from fire exposure thermal response tests. The models calibrated with the experimental char measurements produced the most accurate predictions. The experimental char models validated to predict the behavior of the 1/4 -scale tests within 2.5%, were then able to predict the 1/2 -scale test behavior within 4.5%.