Numerical Investigation of the Influence of a Generator of Vortices on the Supersonic Flow around a Wing

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发表日期：

2024年12月16日

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V. E. Borisov,
T. V. Konstantinovskaya,
A. E. Lutsky

摘要

Abstract

This paper presents the results of a numerical investigation and analysis of the effect of vortex structures from an upstream generator wing on the supersonic flow around the main wing. The effect of the generator wing span is also considered. Numerical results were obtained on a multiprocessor hybrid supercomputer system K-60 at the Keldysh Institute of Applied Mathematics, Russian Academy of Sciences (KIAM RAS).