What Is the Optimal Twist for 3D Printed Micro Wind Turbine Blades?

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SUMMARY

The optimal twist for 3D printed micro wind turbine blades, designed for 5-10 watts output in 30mph wind, requires a non-linear twist distribution. The current design employs a linear twist from 40 degrees at the hub to 85 degrees at the tip, which is not optimal. A more effective approach utilizes the formula twist angle = atan(1/(tsr*x)), where 'x' ranges from 0 at the hub to 1 at the tip, enhancing the twist rate near the hub. Additionally, varying the camber along the blade length is crucial for improved performance, as indicated by research on optimal wind turbine blade design.

PREREQUISITES
  • Understanding of NACA foil shapes and their applications in aerodynamics
  • Knowledge of tip speed ratio (TSR) and its impact on turbine performance
  • Familiarity with 3D printing techniques for creating functional prototypes
  • Basic principles of fluid dynamics as they relate to wind energy conversion
NEXT STEPS
  • Research optimal wind turbine blade design methodologies
  • Explore advanced 3D printing materials suitable for aerodynamic applications
  • Learn about the effects of blade flexing under load and its implications on performance
  • Investigate the relationship between camber variation and efficiency in wind turbine blades
USEFUL FOR

This discussion is beneficial for engineers, designers, and hobbyists involved in renewable energy projects, particularly those focused on optimizing the design and performance of micro wind turbines.

seandepagnier
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how to calculate it?
I am 3d printing micro wind turbine blades (5-10 watts output in 30mph wind), but anyway I am using naca foil shape twisted to make it.

This is not technically a propeller (cannot be efficiently used to push air) because it is generating power from moving air: it is a repeller, but regardless the theory is the same for either, and I need to understand this for making propellers as well.

My question is, how much twist should it have, and how would I calculate the twist correctly?

I have now a linear twist, so starting at 40 degrees at the hub, out to 85 degrees at the tip and it spins really fast in the wind, but it can't be optimal.

When I really think about it, it seems that the twist along the length is non-linear. Meaning it should twist more and more closer to the hub with less rate of change of twist toward the tip. Is this correct? Is it 1/x ? If so, what is the starting twist angle supposed to be?

Further, should the camber or foil shape itself also vary along the length? It seems it should, but how do I calculate this?
 
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The quick, simple, and inferior, method is to use an airfoil cross section and design for constant angle of attack at your design condition. The much better approach is to search optimal wind turbine blade design. That search found a number of good hits, one of which is: https://www.mdpi.com/1996-1073/5/9/3425/pdf. That PDF is highly recommended reading, even if you choose to use the quick and simple method.
 
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I was never using constant angle because this is obviously not going to work well, but I was using a constant twist by twisting linearly which worked pretty well but is not optimal.

Now I have done it piecewise and use the twist angle of atan(1/(tsr*x)) where x is from 0 at hub to 1 at tip and tsr is the tip speed ratio. This gives much more rate of change of twist near the hub, but it's also interesting to see the shape change with different tip speed ratios. I am using 24 segments and it looks smooth. It will be interesting to try it.

I think I can do maybe even better and I"m also wondering about the blade flexing under load, I also need to round the tips, so there is still a lot to experiment
 

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