Lattice Boltzmann method for large eddy simulation of turbulent flows

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The main objective of the study is to assess the capabilities of the lattice Boltzmann method (LBM) for large eddy simulation (LES) of turbulent flows in complex geometries. To this end, an in-house parallel flow solver has been developed to simulate turbulent flows via LBM.The capabilities of the solver are assessed for laminar and turbulent flows by simulating lid-driven cubic cavity flows at different Reynolds numbers. The results obtained with the solver showed physical behaviour that is compatible with the literature. Reinforcing lbmles with the immersed boundary method, bounce back method, and stretched mesh structure applications makes it suitable for complex geometries. Finally, implemented immersed boundary method along with the bounce back schemes are tested for dump combustor geometry and the results are evaluated accordingly.

Original languageEnglish
Title of host publicationAIAA Aviation Forum and ASCEND, 2024
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624107160
DOIs
Publication statusPublished - 2024
EventAIAA Aviation Forum and ASCEND, 2024 - Las Vegas, United States
Duration: 29 Jul 20242 Aug 2024

Publication series

NameAIAA Aviation Forum and ASCEND, 2024

Conference

ConferenceAIAA Aviation Forum and ASCEND, 2024
Country/TerritoryUnited States
CityLas Vegas
Period29/07/242/08/24

Bibliographical note

Publisher Copyright:
© 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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