Detached-Eddy Simulation and Swirl Distortion Characterization of an S-Duct Inlet
Author:
Funder
National Natural Science Foundation of China
Natural Science Foundation of Jiangxi Province
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
https://link.springer.com/content/pdf/10.1007/s13369-022-06827-0.pdf
Reference33 articles.
1. Zhou, Y.-T.; Li, J.; Li, C.-L.; Liu, D.-J.; Li, J.: Influence on compressor characteristic of inlet swirl flow distortion. J. Aerosp. Power 30(8), 1936–1943 (2015). https://doi.org/10.13224/j.cnki.jasp.2015.08.017
2. Tu, B.-F.; Hu, J.: Numerical simulation of low speed axial compressor with swirl distortion. J. Propuls. Technol. 37(9), 1649–1656 (2016)
3. Zachos, P.K.; MacManus, D.G.; Prieto, D.G.; Chiereghin, N.: Flow distortion measurements in convoluted aeroengine intakes. AIAA J. 54(9), 2819–2832 (2016). https://doi.org/10.2514/1.J054904
4. McLelland, G.; Macmanus, D.G.; Zachos, P.K.; Gil-Prieto, D.; Migliorini, M.: Influ- ence of upstream total pressure profiles on s-duct intake flow distortion. J. Propul. Power 36(3), 346–356 (2020). https://doi.org/10.2514/1.B37554
5. Acton, M.J.; Wolff, M.; List, M.G.: Computational Inlet Swirl Distortion Investigation of a High-Speed Compressor, 1–15 (Virtual, Online, 2021).
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