I am doing a project on buckling analysis of Laminated Composites Shell having different cutouts?
At pressurized aircraft cabins, either windscreens and windows are subjected to significant normal loads. Both laminated plate glass or heat-strengthened plate glass can be considered for this kind of application. Laminated plate glass may typically require modulus of elasticity of 70―75 kN/mm2 and bending modulus of rupture of 45 N/mm2, while for heat-strengthened plate glass the modulus of rupture can reach about 200 N/mm2 (*).
(*) H.D Curtis, A. Filippone, M.V. Cook, T.H.G. Megson, M. Tooley BA, D. Wyatt, L.R. Jenkinson, J. Marchman, F. De Florio, J. Watkinson; "Aerospace Engineering Desk Reference", Butterworth-Heinemann (Elsevier), Oxford (UK) and San Diego (USA), 2009, pp. 105-106.
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