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

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

doi:10.2514/6.2017-0075

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 proceeding › Conference 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 language	English
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
ISBN (Electronic)	9781624104473
DOIs	https://doi.org/10.2514/6.2017-0075
Publication status	Published - 9 Jan 2017

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This is the author accepted manuscript (AAM). The final published version (version of record) is available online via AIAA at http://arc.aiaa.org/doi/abs/10.2514/6.2017-0075. Please refer to any applicable terms of use of the publisher.
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Poncet-Montanges, A., Cooper, J., Jones, D., Gaitonde, A., & Lemmens, Y. (2017). Frequency Domain Approach for Transonic Aerodynamic Modelling Applied to a Viscous Wing. In 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference Article AIAA 2017-0075 American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/10.2514/6.2017-0075

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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.",

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Frequency Domain Approach for Transonic Aerodynamic Modelling Applied to a Viscous Wing. / Poncet-Montanges, Adrien; Cooper, Jonathan ; Jones, Dorian et al.
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2017. AIAA 2017-0075.

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

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M3 - Conference Contribution (Conference Proceeding)

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PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

ER -

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

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