Development of an Immersed Boundary Method for High-Speed Compressible Flows

Moran Ezra, Yoram Kozak

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

Abstract

Immersed Boundary Methods (IBM) allow modeling fluid-solid interactions via structured grids. Thus, meshing can be avoided and highly efficient structured grid flow solvers can be utilized. In the current study, we utilize a Ghost Cell Method that relies on interpolation for determining approximate boundary conditions in the ghost cells. However, for high-speed compressible flow regimes, discontinuities in the flow can affect the interpolation accuracy and compromise the solution accuracy and stability. This issue is known to affect highorder interpolations, which can provide superior accuracy for continuous flows. Non-linear interpolation techniques can allow high-order interpolation that is oscillation free. This work introduces an implementation, verification, and validation of a standard low-order interpolation IBM technique in our massively parallel compressible flow solver - Athena-RFX++. Then, for the first time, a new approach for high-order non-linear interpolation based on the Fake Nodes Method is coupled with the IBM. The performance of the Fake Nodes Method is extensively compared against typical low- and high-order interpolation techniques.

Original languageEnglish
Title of host publicationAIAA SciTech Forum and Exposition, 2023
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106996
DOIs
StatePublished - 2023
EventAIAA SciTech Forum and Exposition, 2023 - Orlando, United States
Duration: 23 Jan 202327 Jan 2023

Publication series

NameAIAA SciTech Forum and Exposition, 2023

Conference

ConferenceAIAA SciTech Forum and Exposition, 2023
Country/TerritoryUnited States
CityOrlando
Period23/01/2327/01/23

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