V-22 Osprey

To date, a two dimensional model has been constructed at West Virginia University (WVU) and tested in a Closed Loop Wind Tunnel. The airfoil was placed normal to the airflow using the tunnel air to simulate the vertical component of the downwash experienced in the V-22’s hover mode. Additionally, a long range series of predictive turbulent flow modeling was conducted using state-of-the-art CFD software.