Wake Preservation Using a Coupled Eulerian-Lagrangian Solver

Christopher J A Wales; Dorian P Jones; Ann L Gaitonde

doi:10.2514/6.2022-4087

Wake Preservation Using a Coupled Eulerian-Lagrangian Solver

Christopher J A Wales^*, Dorian P Jones, Ann L Gaitonde

^*Corresponding author for this work

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

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Abstract

A new vortex particle approach seeding approach for a coupled Vortex Particle Method-
Computational Fluid Dynamics solver. The vortex particles are seeded based on the vortcity
flux through a 2D slice in the mesh. Results are presented for a wingtip vortex for the coupled
approach on a coarse mesh and standard CFD on a fine mesh. The affect of particle seeding
resulting on the level of vorticity captured are investigated.

Original language	English
Title of host publication	AIAA AVIATION 2022 Forum
Subtitle of host publication	Session: Other Topics in Computational Fluid Dynamics I
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
ISBN (Electronic)	9781624106354
ISBN (Print)	9781624106354
DOIs	https://doi.org/10.2514/6.2022-4087
Publication status	Published - 27 Jun 2022
Event	AIAA AVIATION Forum - Chicago, United States Duration: 27 Jun 2022 → 1 Jul 2022 https://www.aiaa.org/aviation/

Publication series

Name	AIAA AVIATION 2022 Forum

Conference

Conference	AIAA AVIATION Forum
Country/Territory	United States
City	Chicago
Period	27/06/22 → 1/07/22
Internet address	https://www.aiaa.org/aviation/

Bibliographical note

Funding Information:
This work was carried out within the Clean Sky 2 research programme PERTURB, funded under grant number 831927. The authors gratefully acknowledge the support of Airbus Defence and Space. This work was carried out using the computational facilities of the Advanced Computing Research Centre, University of Bristol-http://www.bristol.ac.uk/acrc/.

Funding Information:
This work was carried out within the Clean Sky 2 research programme PERTURB, funded under grant number 831927. The authors gratefully acknowledge the support of Airbus Defence and Space. This work was carried out using the computational facilities of the Advanced Computing Research Centre, University of Bristol - http://www.bristol.ac.uk/acrc/.

Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA., All rights reserved.

Access to Document

10.2514/6.2022-4087

Full-text PDF (accepted author manuscript)
This is the author accepted manuscript (AAM). The final published version (version of record) is available online via AIAA at https://arc.aiaa.org/doi/abs/10.2514/6.2022-4087. Please refer to any applicable terms of use of the publisher.
Accepted author manuscript, 6.17 MB

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HPC (High Performance Computing) and HTC (High Throughput Computing) Facilities
Alam, S. R. (Manager), Williams, D. A. G. (Manager), Eccleston, P. E. (Manager) & Greene, D. (Manager)
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Cite this

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title = "Wake Preservation Using a Coupled Eulerian-Lagrangian Solver",

abstract = "A new vortex particle approach seeding approach for a coupled Vortex Particle Method-Computational Fluid Dynamics solver. The vortex particles are seeded based on the vortcityflux through a 2D slice in the mesh. Results are presented for a wingtip vortex for the coupledapproach on a coarse mesh and standard CFD on a fine mesh. The affect of particle seedingresulting on the level of vorticity captured are investigated.",

author = "Wales, {Christopher J A} and Jones, {Dorian P} and Gaitonde, {Ann L}",

note = "Funding Information: This work was carried out within the Clean Sky 2 research programme PERTURB, funded under grant number 831927. The authors gratefully acknowledge the support of Airbus Defence and Space. This work was carried out using the computational facilities of the Advanced Computing Research Centre, University of Bristol-http://www.bristol.ac.uk/acrc/. Funding Information: This work was carried out within the Clean Sky 2 research programme PERTURB, funded under grant number 831927. The authors gratefully acknowledge the support of Airbus Defence and Space. This work was carried out using the computational facilities of the Advanced Computing Research Centre, University of Bristol - http://www.bristol.ac.uk/acrc/. Publisher Copyright: {\textcopyright} 2022, American Institute of Aeronautics and Astronautics Inc, AIAA., All rights reserved.; AIAA AVIATION Forum ; Conference date: 27-06-2022 Through 01-07-2022",

year = "2022",

month = jun,

day = "27",

doi = "10.2514/6.2022-4087",

language = "English",

isbn = "9781624106354",

series = "AIAA AVIATION 2022 Forum",

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

booktitle = "AIAA AVIATION 2022 Forum",

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Wales, CJA , Jones, DP & Gaitonde, AL 2022, Wake Preservation Using a Coupled Eulerian-Lagrangian Solver. in AIAA AVIATION 2022 Forum: Session: Other Topics in Computational Fluid Dynamics I., AIAA 2022-4087, AIAA AVIATION 2022 Forum, American Institute of Aeronautics and Astronautics Inc. (AIAA), AIAA AVIATION Forum, Chicago, Illinois, United States, 27/06/22. https://doi.org/10.2514/6.2022-4087

Wake Preservation Using a Coupled Eulerian-Lagrangian Solver. / Wales, Christopher J A ; Jones, Dorian P ; Gaitonde, Ann L.
AIAA AVIATION 2022 Forum: Session: Other Topics in Computational Fluid Dynamics I. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2022. AIAA 2022-4087 (AIAA AVIATION 2022 Forum).

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

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T1 - Wake Preservation Using a Coupled Eulerian-Lagrangian Solver

AU - Wales, Christopher J A

AU - Jones, Dorian P

AU - Gaitonde, Ann L

N1 - Funding Information: This work was carried out within the Clean Sky 2 research programme PERTURB, funded under grant number 831927. The authors gratefully acknowledge the support of Airbus Defence and Space. This work was carried out using the computational facilities of the Advanced Computing Research Centre, University of Bristol-http://www.bristol.ac.uk/acrc/. Funding Information: This work was carried out within the Clean Sky 2 research programme PERTURB, funded under grant number 831927. The authors gratefully acknowledge the support of Airbus Defence and Space. This work was carried out using the computational facilities of the Advanced Computing Research Centre, University of Bristol - http://www.bristol.ac.uk/acrc/. Publisher Copyright: © 2022, American Institute of Aeronautics and Astronautics Inc, AIAA., All rights reserved.

PY - 2022/6/27

Y1 - 2022/6/27

N2 - A new vortex particle approach seeding approach for a coupled Vortex Particle Method-Computational Fluid Dynamics solver. The vortex particles are seeded based on the vortcityflux through a 2D slice in the mesh. Results are presented for a wingtip vortex for the coupledapproach on a coarse mesh and standard CFD on a fine mesh. The affect of particle seedingresulting on the level of vorticity captured are investigated.

AB - A new vortex particle approach seeding approach for a coupled Vortex Particle Method-Computational Fluid Dynamics solver. The vortex particles are seeded based on the vortcityflux through a 2D slice in the mesh. Results are presented for a wingtip vortex for the coupledapproach on a coarse mesh and standard CFD on a fine mesh. The affect of particle seedingresulting on the level of vorticity captured are investigated.

U2 - 10.2514/6.2022-4087

DO - 10.2514/6.2022-4087

M3 - Conference Contribution (Conference Proceeding)

SN - 9781624106354

T3 - AIAA AVIATION 2022 Forum

BT - AIAA AVIATION 2022 Forum

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

T2 - AIAA AVIATION Forum

Y2 - 27 June 2022 through 1 July 2022

ER -

Wake Preservation Using a Coupled Eulerian-Lagrangian Solver

Abstract

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Bibliographical note

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Equipment

HPC (High Performance Computing) and HTC (High Throughput Computing) Facilities

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