Comparison of the Buckling Performance of Grid Stiffened and Sandwich Structures designed for Wind Turbine Blade Trailing Panels

Master Thesis (2018)
Author(s)

Remko de Ronde (TU Delft - Aerospace Engineering)

Contributor(s)

Julien van Campen – Mentor (TU Delft - Aerospace Structures & Computational Mechanics)

Sonell Shroff – Mentor (TU Delft - Aerospace Manufacturing Technologies)

F. Lahuerta Calahorra – Mentor (Knowledge Centre WMC)

Roeland De Breuker – Graduation committee member (TU Delft - Aerospace Structures & Computational Mechanics)

Julie Teuwen – Graduation committee member (TU Delft - Aerospace Manufacturing Technologies)

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Publication Year
2018
Language
English
Graduation Date
23-02-2018
Awarding Institution
Programme
Aerospace Engineering
Sponsors
Knowledge Centre WMC
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Abstract

Future wind turbines require larger rotor blade radius, leading to an increase of rotor swept area. The larger rotor swept area results in more energy production of the wind turbine. Further increase is however limited as a result of the structural weight, which induces a large bending moment and could result in buckling of the rotor blade. An innovative design solution resulting in a lower weight blade design could be acquired by introducing a grid stiffened structure as a substitution of the conventional sandwich structure. Design and analysis showed an increase in specific stiffness of the grid stiffened structure for higher loading conditions. In an attempt to validate the obtained results, one sandwich and one orthogrid panel has been manufactured and tested.

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