Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling applied to a 3D Wing

Adrien Poncet-Montanges, J. E. Cooper, D. Jones, A. L. Gaitonde, Y. 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 applied to a wing, the reduced order model shows a strong ability to reconstruct the full order frequency response of the lift and pitching moment. Based on a 2D method, the wing is sliced in different strips; a sensitivity analysis is carried out on each strip and on the total forces and moments to understand the influence of some parameters on the accuracy of the model.
Original languageEnglish
Title of host publicationAIAA Modeling and Simulation Technologies Conference, 2016
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages20
ISBN (Print)9781624104299
DOIs
Publication statusPublished - 13 Jun 2016
EventAIAA Modeling and Simulation Technologies Conference, 2016 - Washington, United States
Duration: 13 Jun 201617 Jun 2016

Conference

ConferenceAIAA Modeling and Simulation Technologies Conference, 2016
CountryUnited States
CityWashington
Period13/06/1617/06/16

Structured keywords

  • ALPES

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