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Final report for WP4.3: Enhancement of design methods ... - Upwind

Final report for WP4.3: Enhancement of design methods ... - Upwind

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In every time step the system matrices <strong>of</strong> Flex5, i.e. mass M, stiffness S, damping D, and the current loading<br />

F is transferred to the finite element code. There the models are combined on the level <strong>of</strong> equations <strong>of</strong><br />

motion and the hydrodynamic loads are added. The equations are solved in the finite element code. The<br />

results, i.e. displacements, velocities and accelerations ( x, x&,<br />

&x<br />

&)<br />

are used in Flex5 to update the geometry,<br />

the loading and the controls. Figure 2.2 shows the coupling process and data exchange.<br />

Flex5<br />

FE-Code<br />

t n-1<br />

t n-1<br />

Newmark<br />

Solver<br />

x, x& , && x<br />

13<br />

t n<br />

t n<br />

M Flex , D Flex ,<br />

S Flex, F Aero<br />

Newmark<br />

Solver<br />

t n+1<br />

t n+1<br />

shared memory or<br />

DLL interface<br />

Figure 2.2: Process <strong>of</strong> the full integrated coupling between Flex5 and a finite element code [7]<br />

Three full integrated couplings have been realized: Flex5-FECOS [6], Flex5-Poseidon and Flex5-ASAS<br />

[7]. The first one was created within UpWind, the two other couplings have been created in the Project<br />

OWEA - Verification <strong>of</strong> <strong>of</strong>fshore wind turbines [8]. The interface and the modelling capabilities are different<br />

between the tools, but the coupling method is the same. FECOS is a finite element code compiled as a<br />

dynamic link library (DLL) and is included in Flex5 directly. There<strong>for</strong>e no special interface is necessary to<br />

handle the data exchange. Flex5-Poseidon uses a shared memory interface where both tools access the<br />

same memory. Flex5-ASAS uses a separate DLL <strong>for</strong> the data exchange.<br />

Advantages and disadvantages<br />

An important advantage <strong>of</strong> the full integrated coupling is that specific simulation codes are combined without<br />

losing their potential. The application possibility <strong>of</strong> the coupled tools has been extended. The method<br />

considers dynamic effects between the wind turbine and the support structure. The load calculation takes<br />

relative velocities <strong>of</strong> the entire structure into account. Non-linear problems can also be simulated using<br />

Flex5-ASAS.<br />

The main disadvantage is the computational time. The simulation speed is lower than the sequential approach<br />

and much lower than a Flex5 stand-alone simulation. The reasons <strong>for</strong> this can be found in the<br />

large number <strong>of</strong> freedoms and the data exchange between the tools in every time step. The simulation<br />

speed can be increased if a reduction method is implemented in the finite element code, but this restricts<br />

the simulations to linear problems.<br />

2.2 Combined multi-body / modal approach<br />

This section describes the GH Bladed s<strong>of</strong>tware code as an example <strong>of</strong> an integrated <strong>design</strong> tool <strong>for</strong> calculating<br />

wind turbine per<strong>for</strong>mance and dynamic response [9]. Bladed was originally developed <strong>for</strong> the modelling<br />

<strong>of</strong> onshore fixed-bottom wind turbines, but has been extended to include hydrodynamic loading <strong>for</strong> the<br />

modelling <strong>of</strong> <strong>of</strong>fshore wind turbines. In the last year the core structural dynamic calculation in the code has<br />

been extended to incorporate multibody dynamics.<br />

The Bladed code uses a modal representation to model the structural dynamics <strong>of</strong> a wind turbine. This<br />

approach has the major advantage <strong>of</strong> giving an accurate and reliable representation <strong>of</strong> the dynamics <strong>of</strong> a<br />

wind turbine with relatively few degrees <strong>of</strong> freedom, making it a fast and efficient means <strong>of</strong> computation. In<br />

the previous version <strong>of</strong> the Bladed code, the modal properties <strong>of</strong> the rotating and non-rotating components<br />

<strong>of</strong> the system (i.e. the rotor and tower) were computed independently using a finite element representation<br />

<strong>of</strong> the structure, then coupled together using the appropriate equations <strong>of</strong> motion in the dynamic response

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