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Bent F. Sørensen's picture

PhD position at the Technical University of Denmark (DTU) in solid mechanics and fracture mechanics of composite materials

We have an open position as a PhD student in the area of fracture mechanics of fibre composites. The focus of the position is to develop element test specimens, i.e., test specimens that are purposely-designed with the aim of checking the accuracy of model predictions of damage evolution (two or more damage types) in composite structures subjected to static and cyclic loading

Postdoc vacancy (3 years) on computational mechanics of thick adhesive joints in large wind turbine blades

Over the last years, UGent-MMS has developed the stand-alone BladeMesher software for generating finite element models of large wind turbine blades. The software reads in the material data and airfoil data of the wind turbine blade, and automatically constructs the geometry and finite element mesh for the blade. In a next step, the nodal and element information of the finite element mesh is written out to an input file for a commercial finite element solver (Abaqus in this case).

PhD/postdoc vacancy (4 years) on computational mechanics of large wind turbine blades

Over the last years, UGent-MMS has developed the stand-alone BladeMesher software for generating finite element models of large wind turbine blades. The software reads in the material data and airfoil data of the wind turbine blade, and automatically constructs the geometry and finite element mesh for the blade. In a next step, the nodal and element information of the finite element mesh is written out to an input file for a commercial finite element solver (Abaqus in this case).

Non-linear Buckling in Ansys

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Hello to all,

                 I m mahendra and i want few suggesions for my final year project Regarding Non-Linear buckling of composite Wind Turbine. I have done Linear Buckling and got a BLF=1.3 which is fine as per GL Guidlines. I m using Ansys12 Edu ver. and Shell 281 Element type with section properties. For load application i m using pilot node at 9 airfoils on the full blade.

Then i have applies Mx and My on that load application points.

In Non-Linear Analysis i m not getting the convergence as i m applying load on one node or at all the 9 points.

allanwood's picture

VABS 3.6 Reduces Realistic Composite Blade Modeling to Seconds

AnalySwift, LLC, a leading provider of efficient high-fidelity modeling software for aerospace and energy composites and other advanced materials, announced today the release of VABS 3.6. This is the latest version of VABS, which is the tool of choice for efficient and accurate modeling of composite slender structures such as wind turbine blades, helicopter rotor blades, high aspect ratio wings, composite bridges, and other slender structural components.

Bent F. Sørensen's picture

Deadline is approaction: 10 april - "Risø Int. Symposium: Composite materials for structural performance: towards higher limits"

The deadline for abstract submission for the 32, 10th April 2011, is approaching. The title of the 32nd Risø International Symposium on Materials Science is "Composite materials for structural performance: towards higher limits". The Symposium will be held from Monday 5th September to Friday 9th September 2011 at Risoe DTU - National Laboratory for Sustainable Energy, Technical University of Denmark, 4000 Roskilde, Denmark. We think this is an exciting Symposium theme and we are proud to present a great list of key-note presentations:

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