Titlebook: Buckling and Postbuckling of Composite Plates; G. J. Turvey,I. H. Marshall Book 1995 Chapman & Hall 1995 buckling.deformation.finite eleme

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https://doi.org/10.1007/978-1-349-86035-7. Design parameters such as layer thicknesses and ply angles can be employed to great effect to achieve an optimized structure with improved weight and stiffness characteristics. This chapter deals with the lay-up optimization of laminated plates subject to buckling loads. A survey of the subject is

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Understanding the good and the bad,This chapter is a review of the AFIT work and will discuss both its experimental and analytical features. Other organizations have pursued similar research [., .] and the AFIT work has cited their findings. AFIT is the only organization that has continued to explore many of the intricacies of this i

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Shear deformation and sandwich configurationClassical plate theory (CPT) is generally credited to Kirchhoff over 125 years ago.

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William Buchanan BSc, CEng, Phdimportance. For example, composite plate-like subcomponents with cut-outs are being considered for use in many types of aerospace structures owing to their high stiffness-to-weight and strength-to-weight properties. These properties could ultimately yield substantial weight savings for aircraft structures.

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