The main goals of the simulation platform can be summarized as follows: 1) To extend the ability of the existing wind turbine design tools to simulate the dynamic behavior of the wind turbines and the
The objective of the project was an improved design base for extreme loads and fatigue loads on wind turbine in flat or mountainous terrain. The main activity was the development of models for non
The aim of the project is to develop better design basis for large wind turbine blade of composite materials by a combination of materials research, structural mechanics, involving both modelling and
The main objectives are the following: a) development of a design tool for analysis of dynamic stability. b) investigations of blade tip aerodynamics and blade tip design on basis of 3D CFD
This pre-project had the aim of establishing the basic technical knowledge to evaluate whether remote surveillance of the rotor blades of large off-shore wind turbines has technical and economical
Ice loading on wind turbine foundations is a design load in the inner Danish seas and straits. Relatively conservative design requirements/guidelines have so far been used for prediction of ice loads
The aim of the project was to analyze the environmental effects of wind turbines during manufacturing and after disposal in a long term perspective and to give societal recommendations in relation to
The purpose of the project is to verify, refine and develop micrometeorological tools for the estimation of load-critical wind conditions in landscapes in Denmark and Europe, where wind turbines (and
The aims of the project was enhancing and further developing a model system capable of analysing and predicting the wind and the potential wind energy in Denmark.
The overall objective with the project has been to develop and verify a model for assessment of the interaction between a wind farm and the power systern.
The project has comprised the following six milestones: a) status on 2D and 3D CFD computations, b) implementation of improved aerodynamic and structural sub models in the aeroelastic codes FLEX4 and