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.
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 |
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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 | |
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 |
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Conference
Conference | AIAA AVIATION Forum |
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Country/Territory | United States |
City | Chicago |
Period | 27/06/22 → 1/07/22 |
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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Alam, S. R. (Manager), Williams, D. A. G. (Manager), Eccleston, P. E. (Manager) & Greene, D. (Manager)
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