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A website for discussions on wind turbine basic theory, mathematical analysis, wind tunnel testing, and test model building with emphasize on Darrieus rotor.

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Analyse : Multiple streamtube model, [pg2], [code] | single streamtube | Glauert empirical formula | about Naca airfoils data | finite aspect ratio on airfoil, [code] | dimensionless analysis on Darrieus rotor efficiency

Single streamtube model for Darrieus rotor

The single streamtube model is very different from the multiple streamtube model in term of the calculation method (or equations) and the velocity field. The multiple streamtube assumed a very simple one-direction velocity field (i.e. velocity varies in 2 axis) in the rotor but the single streamtube model is even simpler as the velocity field is replaced by only a single velocity value. Weird enough, the resulting power coefficient curve does not seems to differ too much except that single streamtube seem to over predict slightly.

In single streamtube model, the flow through the rotor is modeled using one single streamtube only as its name imply. The streamtube cross-section area (swept area) remains constant and follows a straight path just like the multiple streamtubes model. The wind speed decrease from upstream velocity, U to velocity at rotor, U’ and finally settle down at far downstream velocity. The velocity remains constant like previous model when moving though the circular blade path.

The only streamtube experiences aerodynamics forces all the time as opposed to pulses of forces in multiple streamtube. The variation of aerodynamic forces are large in the whole revolution from 0 to 360 degree, so the single tube model has to sum up all the forces at various position to average the value off before equating it to the wind momentum loss rate.

Similarly, the induction factor for single streamtube model also has to be solved numerically by root finding algorithm but for one single value only. However, to find the first thrust coefficient (derived from aerodynamic force), the value of the normalized velocity, angle of attack, lift, drag, normal, and tangent coefficient for a set of predetermined blade position (theta) which cover the whole revolution have to be obtained first before the summation and averaging is carried using the above equation. So, even though only one value of induction factor is needed, the number of loop seems to remain at 2 roughly. Once the induction factor for the single streamtube is found, the torque and power coefficients can be calculated using the same previous set of equations.

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Last updated at November 6, 2002
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