H2020 ENODISE: Numerical Aeroacoustic Database Configuration A1 : GPUP

This dataset contains the numerical prediction for A1 configuration as defined in the H2020 ENODISE project (https://www.vki.ac.be/index.php/about-enodise). In this configuration, a single two-bladed propeller is immersed in a boundary layer. The present results can be compared to the measurements carried out by the University of Bristol.

 The investigated operating point as calculated in the prediction is:

• Uinf = 33 m/s, 6500 rpm, advance ratio J=1

The results were calculated using the LES-CABARET method on GPUs. The results presented are preliminary result on coarse grid with the comparison with the experiment for hot-wire and overhead acoustic data at 60-, 90- and 120-degree observer angles.