Flow Development Through An S-Shaped Diffusing Duct
Author:
Affiliation:
1. School of Aeronautics and Astronautics , Shanghai Jiao Tong University , Shanghai , China
2. AECC Commercial Aircraft Engine Company , Shanghai , China
Abstract
Publisher
Walter de Gruyter GmbH
Subject
Aerospace Engineering
Link
https://www.degruyter.com/document/doi/10.1515/tjj-2019-0045/pdf
Reference21 articles.
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2. Gräsel J, Pierré M, Demolis J. Parametric interturbine duct design and optimisation. Int Congr Aeronaut Sci (ICAS). ICAS 2006-5.1.2, 2006.
3. Jin D, Liu X, Zhao W, Gui X. Optimization of endwall contouring in axial compressor S-shaped ducts. Chin J Aeronaut. 2015;28:1076–86.
4. Garnier E, Leplat M, Monnier JC, Delva J. Flow control by pulsed jet in a highly bended S-duct. 6th AIAA Flow Control Conference, AIAA-2012-3250, 2012.
5. Garnier E. Flow control by pulsed jet in a curved S-duct: a spectral analysis. Aiaa J. 2015;53:2813–27.
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2. Performance enhancement and flow separation control in an S-duct by air injection;International Journal of Turbo & Jet-Engines;2022-05-12
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