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

Adrien Poncet-Montanges, Jonathan Cooper, Dorian Jones, Ann Gaitonde, Yves Lemmens

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

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Abstract

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.
Original languageEnglish
Title of host publication58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages16
ISBN (Electronic)9781624104473
DOIs
Publication statusPublished - 9 Jan 2017

Structured keywords

  • ALPES

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