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A Novel Full-scale Validation of Thermal Degradation of Polymer Foam Cored Sandwich Structures R.K. Fruehmann, J.M. Dulieu-Barton, O.T. Thomsen15.02. 2011
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2 Outline Background Review of design brief Design for mechanical boundary conditions Thermal gradient measurement Validation tests Conclusions
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3 Background EC1EC1 EC2EC2 E C1 < E C2 PVC foam core Metal or composite face sheet T out T in
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4 Background Thermal degradation of PVC foam stiffness
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5 Background Face sheet displacement at different loads Force / mid-span displacement results from 3 different models (Frostig et al. 2004) High-order sandwich panel theory (HSAPT) predicts strongly non-linear interactions between mechanical and thermal loads. Strongly non-linear and unstable load response and limit point behaviour in some cases. Load response strongly sensitive to boundary conditions. Experimental validation is required.
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6 Design Brief Mechanical 1.Simply supported 2.Lower corner fixed – free to rotate 3.Fully clamped Thermal 1.Uniform across width 2.Linear through thickness Measurement 1.Non-contact (DIC & IR) Condition 1 Condition 2 Condition 3
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7 Design space Loading frame Actuator 3 point bend rig Load cell
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8 Design – End constraint fixture Platform Fork Specimen clamp Axis CG Counter balance
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9 Face sheet thickness Design – End constraint fixture Axis Height adjustment Platform height
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10 Design – Boundary condition 3
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11 Design – Boundary condition 3 Main platform shaft Platform Axis Fixation bolt Vertical supports
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12 Design – General arrangement Radiator Insulation Mirror to monitor top face sheet Mirror to monitor bottom face sheet
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13 Thermal gradient
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14 Thermal gradient
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15 Thermal gradient
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16 Thermal gradient
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17 Thermal gradient Thermal degradation of PVC foam stiffness
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18 Thermal gradient Thermal degradation of PVC foam stiffness
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19 Thermal gradient Thermal degradation of PVC foam stiffness
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20 Validation tests Specimen dimensions: –450 x 50 x 27 mm –1 mm thick aluminium face sheets –25 mm thick H100 PVC foam Temperature profile across the width and through the thickness Recorded the deformations at the mid-span using DIC
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21 Thermal gradient 1 second 5 seconds 10 seconds 15 seconds
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22 Thermal gradient
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23 Mid-span deformation 1 2
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24 Mid-span deformation
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25 Mid-span deformation
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26 Mid-span deformation Careful consideration of face sheet failure loads to avoid indentation failure preceding geometric non-linearity.
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27 Conclusions Thermal and mechanical boundary conditions have been achieved. Mid-span deflections correspond qualitatively with model predictions for the simply supported case.
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28 Future challenges Optimise specimen configuration (material and geometry) to remain in the elastic region. Obtain DIC data from the thin face sheets. Obtain DIC data below the roller during indentation.
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Thank you
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