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On the estimation of the shear modulus of a honeycomb sandwich panel from X-ray mapping of its core.
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Honeycomb sandwich panels are widely used in the industry because of their outstanding stiffness to mass ratios. The dynamic response of such structures is known to be relatively complex especially in the mid-frequency domain where a strong orthotropy can be observed. Several equivalent models are available in the literature to understand and predict this behavior, all relying on an assumption that the geometry of the honeycomb core is periodic and perfectly known. The effect of imperfection inevitably introduced at the manufacturing stage are characterized in this work using X-ray measurements. A simple homogenization approach is proposed, allowing the prediction of the shearing properties of the core from statistics extracted from its geometry. These properties are used to predict the dynamic behavior of the structure using a multi-layer analytical model. Results are compared to Laser Doppler Vibrometer measurements, showing a very good agreement with the predictions based on X-ray pictures.
To cite this article
About: Q. Leclère
Univ Lyon, INSA-Lyon, LVA EA677, F-69621 Villeurbanne, France
About: K. Ege
Univ Lyon, INSA-Lyon, LVA EA677, F-69621 Villeurbanne, France
About: F. Marchetti
Matelys - Research Lab, F-69120 Vaulx-en-Velin, France
About: N.B. Roozen
Laboratory for Acoustics, Soft Matter and Biophysics, Department of Physics and Astronomy, KU Leuven, Celestijnenlaan 200D,
B3001 Heverlee, Belgium
About: Ph. Duvauchelle
Univ Lyon, INSA-Lyon, LVA EA677, F-69621 Villeurbanne, France
About: M. Tahraoui
Univ Lyon, INSA-Lyon, LVA EA677, F-69621 Villeurbanne, France
About: V. Kaftandjian
Univ Lyon, INSA-Lyon, LVA EA677, F-69621 Villeurbanne, France