Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling

A P Poncet-Montanges; Jonathan E Cooper; Dorian Jones; Ann L Gaitonde; Y Lemmens

doi:10.2514/6.2016-1576

Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling

A P Poncet-Montanges, Jonathan E Cooper, Dorian Jones, Ann L Gaitonde, Y 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 from the TAU linearized frequency domain solver for a NLR7301 airfoil in the transonic domain, the reduced order model shows a strong ability to reconstruct the full order frequency response. On the other hand, the model built in the frequency domain gives promising results when applied to reconstruct nonperiodic motions, as a 1-cos pitching. Compared to a time domain simulation, the lift and the pitching moment obtained are accurate, even with small sizes for the reduced order model, and with a substantial gain of calculation time.

Original language	English
Title of host publication	15th Dynamics Specialists Conference
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages	13
ISBN (Electronic)	9781624103988
DOIs	https://doi.org/10.2514/6.2016-1576
Publication status	Published - 4 Jan 2016
Event	15th Dynamics Specialists Conference, 2016 - San Diego, United States Duration: 4 Jan 2016 → 8 Jan 2016

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Conference	15th Dynamics Specialists Conference, 2016
Country/Territory	United States
City	San Diego
Period	4/01/16 → 8/01/16

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ALPES

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10.2514/6.2016-1576

SciTech2016_AdrienPoncet-MontangesAccepted author manuscript, 837 KB

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title = "Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling",

abstract = "This work introduces a method for the construction of a reduced order model in the frequency domain. With input data obtained from the TAU linearized frequency domain solver for a NLR7301 airfoil in the transonic domain, the reduced order model shows a strong ability to reconstruct the full order frequency response. On the other hand, the model built in the frequency domain gives promising results when applied to reconstruct nonperiodic motions, as a 1-cos pitching. Compared to a time domain simulation, the lift and the pitching moment obtained are accurate, even with small sizes for the reduced order model, and with a substantial gain of calculation time.",

author = "Poncet-Montanges, {A P} and Cooper, {Jonathan E} and Dorian Jones and Gaitonde, {Ann L} and Y Lemmens",

year = "2016",

month = jan,

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doi = "10.2514/6.2016-1576",

language = "English",

booktitle = "15th Dynamics Specialists Conference",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

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note = "15th Dynamics Specialists Conference, 2016 ; Conference date: 04-01-2016 Through 08-01-2016",

}

Poncet-Montanges, AP, Cooper, JE , Jones, D , Gaitonde, AL & Lemmens, Y 2016, Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling. in 15th Dynamics Specialists Conference., AIAA 2016-1576, American Institute of Aeronautics and Astronautics Inc. (AIAA), 15th Dynamics Specialists Conference, 2016, San Diego, United States, 4/01/16. https://doi.org/10.2514/6.2016-1576

Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling. / Poncet-Montanges, A P; Cooper, Jonathan E ; Jones, Dorian et al.
15th Dynamics Specialists Conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2016. AIAA 2016-1576.

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

TY - GEN

T1 - Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling

AU - Poncet-Montanges, A P

AU - Cooper, Jonathan E

AU - Jones, Dorian

AU - Gaitonde, Ann L

AU - Lemmens, Y

PY - 2016/1/4

Y1 - 2016/1/4

N2 - This work introduces a method for the construction of a reduced order model in the frequency domain. With input data obtained from the TAU linearized frequency domain solver for a NLR7301 airfoil in the transonic domain, the reduced order model shows a strong ability to reconstruct the full order frequency response. On the other hand, the model built in the frequency domain gives promising results when applied to reconstruct nonperiodic motions, as a 1-cos pitching. Compared to a time domain simulation, the lift and the pitching moment obtained are accurate, even with small sizes for the reduced order model, and with a substantial gain of calculation time.

AB - This work introduces a method for the construction of a reduced order model in the frequency domain. With input data obtained from the TAU linearized frequency domain solver for a NLR7301 airfoil in the transonic domain, the reduced order model shows a strong ability to reconstruct the full order frequency response. On the other hand, the model built in the frequency domain gives promising results when applied to reconstruct nonperiodic motions, as a 1-cos pitching. Compared to a time domain simulation, the lift and the pitching moment obtained are accurate, even with small sizes for the reduced order model, and with a substantial gain of calculation time.

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DO - 10.2514/6.2016-1576

M3 - Conference Contribution (Conference Proceeding)

AN - SCOPUS:84958087420

BT - 15th Dynamics Specialists Conference

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

T2 - 15th Dynamics Specialists Conference, 2016

Y2 - 4 January 2016 through 8 January 2016

ER -

Frequency Domain Approach for Transonic Unsteady Aerodynamic Modelling

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