A parametric study for panel buckling sensitivity of composite sandwich wind turbine blades
Date of Award
2011
Degree Name
M.S. in Civil Engineering
Department
Department of Civil and Environmental Engineering and Engineering Mechanics
Advisor/Chair
Advisor: Steven L. Donaldson
Abstract
A parametric study of buckling performance of composite wind turbine blade regions with thin symmetric laminated sandwich rectangular panels, subjected to uniform axial shell edge compression loads is presented. The research primarily focused on the critical buckling strain level and with nondimensional core material parameters, such as transverse core shear modulus and core thickness, for rectangular sandwich strips with sufficiently long aspect ratio. Both flat and curved-section models representing different regions of the blade were considered. Extensive buckling-design plots, based on fixed sets of laminate designs and critical buckling loads, provide an insight on optimal core solutions. Several typical buckling response sweeps are presented and discussed in this paper to illustrate easy to understand and useful design findings.
Keywords
Turbines Blades Design and construction Testing, Buckling (Mechanics), Materials Compression testing
Rights Statement
Copyright © 2011, author
Recommended Citation
Miao, Shicong, "A parametric study for panel buckling sensitivity of composite sandwich wind turbine blades" (2011). Graduate Theses and Dissertations. 442.
https://ecommons.udayton.edu/graduate_theses/442