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 proceedingConference 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 languageEnglish
Title of host publicationAIAA AVIATION 2022 Forum
Subtitle of host publicationSession: Other Topics in Computational Fluid Dynamics I
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
ISBN (Electronic)9781624106354
ISBN (Print)9781624106354
DOIs
Publication statusPublished - 27 Jun 2022
EventAIAA AVIATION Forum - Chicago, United States
Duration: 27 Jun 20221 Jul 2022
https://www.aiaa.org/aviation/

Publication series

NameAIAA AVIATION 2022 Forum

Conference

ConferenceAIAA AVIATION Forum
Country/TerritoryUnited States
CityChicago
Period27/06/221/07/22
Internet address

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.

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