Rotor Blade Aeroelasticity
Rotor Blade Aeroelasticity (RBA) simulations model the aerodynamic performance of elastic rotor blades using displacement and twist data from external files. You can create these data files in multi-body dynamics software such as RCAS, CAMRAD-II, DYMORE, and FLIGHTLAB. Typical RBA applications include urban air vehicle rotors, wind turbines, and helicopter rotors.
The external software models a rotor blade as a 1D beam and collects the beam displacement data. The data consists of three translational and three rotational deformations at various control points on the beam as the rotor rotates. Simcenter STAR-CCM+ applies the external beam data to the fluid boundaries at the fluid-blade interface and computes the corresponding fluid loads.
- A background region for the fluid far from the rotating blade. This region contains the entire simulation domain and is enclosed by a free stream boundary in which the air speed is applied as a boundary condition.
- An overset region for each rotor blade. These regions model the fluid around the rotating blades. They are enclosed by the overset boundaries and contain the fluid wall boundaries at the fluid-blade interface.
