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The present work analyzes the three-dimensional unsteady flow structure of a low-speed low-pressure ratio axial fan stage operating at stall conditions. Unsteady numerical simulations were conducted with the elsA software, which solves the unsteady R
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::eea54e66d1ba6380d82c6303f38277e3
https://oatao.univ-toulouse.fr/29401/
https://oatao.univ-toulouse.fr/29401/
Autor:
Rojda, Ludovic
Publikováno v:
Autre. Université de Lyon, 2020. Français. ⟨NNT : 2020LYSEC038⟩
Compressor performance and operability are continuously improving to obtain a more efficient aeronautical engine. Indeed, during transient phases of aircraft’s flight path, the compressor is a critical element. Therefore, accurate prediction of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::1b99aab29cd4c95981082ce14f92095f
https://tel.archives-ouvertes.fr/tel-03237680/document
https://tel.archives-ouvertes.fr/tel-03237680/document