Hello,
In the documentation about Aerodyn module, it is mentioned that:
AeroDyn calculates aerodynamic loads on both the blades and tower. Aerodynamic calculations within AeroDyn are based on the principles of actuator lines,
This is confusing, because the actuator line method by design can work only with a computational domain (requires a CFD solver). As an example, I quote this (from this PhD thesis):
The actuator line method, introduced by Sørensen and Shen [75], is a fully three-dimensional
and unsteady aerodynamic model for studying the flow field around wind turbines. The method combines a three-dimensional Navier-Stokes solver with a so-called actuator line technique in which body forces are distributed radially along lines representing the blades of the wind turbine.
Could you please clarify the confusion? I assume that documentation is referring to “Actuator disc” concept (for example, as explained here) not “Actuator line”?
In addition, the current documentation seems to contradict the old Theory manual (link: https://www.nrel.gov/docs/fy05osti/36881.pdf). The Theory manual explicitly explains the Actuator disk concept (starting from page 13 of the PDF file).
Best regards,