This paper presents the wind tunnel test results from MEXNEXT, an IEA wind task for analyzing the measurements which have been taken in the EU project ‘MEXICO’. A 2/4.5 scaled model of ‘MEXICO’ rotor was tested in the KARI low wind tunnel with 5 × 3.75 m2 open jet test section. The...

The aerodynamic performance of the ‘NREL Phase VI’ rotor with a 2 m diameter was tested in the open jet test section. The original rotor with a 10.06 m diameter was tested in the NASA Ames tunnel and the test result was used as validation data for the computational model. The Reynolds...