Development and validation of a method to predict non-linear aerodynamic characteristics of lifting surfaces with controls

The purpose of this research proposal is to develop numerical methods for the prediction of the non-linear aerodynamic characteristics of lifting surfaces, of the type used in the tails of commercial aircraft. The maximum lift coefficient of the lifting surface, including deflected controls, is of interest for the design of efficient empennages and a rapid means to estimate this parameter is required. The methods to be developed will be calibrated and validated using a systematic series of wind tunnel tests of several models covering a wide range of planform parameters, with and without simulated ice shapes. Please refer to the full topic descriptions document published in this call.