Hi, I’m trying to reproduce some controllers of nrel.gov/wind/pdfs/42437.pdf (page 21); through a mathematical model, so I need to work with the same Cp versus TSR and pitch surface (to compare) for the CART, which can be obtained by means simulation using the aerodynamic code WT_Perf. Which yaw error value I have to use?
It is assumed that Cpmax = 0.3659 (from nrel.gov/wind/pdfs/42437.pdf), which was determined to be -1 deg and TSR = 7.5.
Thanks in advance.
Regards.
Jován Mérida.