@inproceedings{17bb0fcf835d4f22a87cef65ff0e9374,
title = "Experimental characterization of flow distortion in a semi-embedded engine intake for boundary layer ingestion application",
abstract = "ONERA conducted wind tunnel tests on a generic boundary layer ingestion setup, in the framework of the SUBLIME research program, in the S3Ch continuous transonic facility. The objective of this project funded by the French Ministry of Civil Aviation (DGAC) is to characterize the distortion of the flow in the fan plane. These experimental measurements provide a better knowledge of the heterogeneities present in the flow seen by the turbojet with boundary layer ingestion. The experimental database is very useful for the benchmarking of numerical simulation tool over a complex flow configuration.",
author = "N. Rembaut and O. Atinault and V. Brion",
note = "Publisher Copyright: {\textcopyright} 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023 ; Conference date: 12-06-2023 Through 16-06-2023",
year = "2023",
month = jan,
day = "1",
doi = "10.2514/6.2023-3255",
language = "English",
isbn = "9781624107047",
series = "AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023",
}