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.
|Title of host publication||58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference|
|Publisher||American Institute of Aeronautics and Astronautics Inc. (AIAA)|
|Number of pages||16|
|Publication status||Published - 9 Jan 2017|