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Hi,
What is the best way to design the root region of a wind turbine blade (for a small model turbine: 0.7m diameter, Re ~ 10,000)? So far we've selected our airfoil and calculated the chord lengths (proprtional to 1/R) but can't find any mathematics on the root region. At what point should it cease to follow the 1/r relationship and should this be a fairly abrupt change or a curved gradual change?
Furthermore, what is teh best way to calculate the bending stresses at the root
Thanks for any help
What is the best way to design the root region of a wind turbine blade (for a small model turbine: 0.7m diameter, Re ~ 10,000)? So far we've selected our airfoil and calculated the chord lengths (proprtional to 1/R) but can't find any mathematics on the root region. At what point should it cease to follow the 1/r relationship and should this be a fairly abrupt change or a curved gradual change?
Furthermore, what is teh best way to calculate the bending stresses at the root
Thanks for any help