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AN IMMERSED BOUNDARY METHOD FOR THE CFD SOLVER AIRBUS-CODA
Publicated to:World Congress In Computational Mechanics And Eccomas Congress. - 2022-01-01 (), DOI: 10.23967/eccomas.2022.047
Authors: Llorente VJ; Lodares D; Ferrer E; Valero E
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Abstract
This work implements and analyses an Immersed Boundary Method based on Volume Pezalization for the flow simulator Airbus-CODA (CFD for ONERA, DLR, and AIRBUS). The Immersed Boundary Volume Penalization has unique advantages, e.g. easy to implement, straightforward formulation for moving geometries, and numerical errors can be controlled a- priori [1, 2], showing the potential for aeronautical applications. Numerical experiments will assess the accuracy of the Immersed Boundary Volume Penalization in CODA.
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Bibliometric impact. Analysis of the contribution and dissemination channel
The work has been published in the journal World Congress In Computational Mechanics And Eccomas Congress, Q4 Agency Scopus (SJR), its regional focus and specialization in Mechanical Engineering, give it significant recognition in a specific niche of scientific knowledge at an international level.
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Leadership analysis of institutional authors
This work has been carried out with international collaboration, specifically with researchers from: Germany.
There is a significant leadership presence as some of the institution’s authors appear as the first or last signer, detailed as follows: First Author (LLORENTE LAZARO, VICTOR JAVIER) and Last Author (VALERO SANCHEZ, EUSEBIO).