Frequency Domain Approach for Transonic Aerodynamic Modelling Applied to a Viscous Wing

摘要

This work introduces a method for the construction of a reduced order model in the frequency domain. With input data obtained with the TAU linearized frequency domain solver, the reduced order model shows a strong ability to reconstruct the full order frequency response of a viscous aircraft configuration. Reduced order models have been successfully created for different strips on the wing, the fuselage and the horizontal plane.