Influence of an upstream transonic axial compressor stage on the performance of inter-stage duct
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials
Link
https://link.springer.com/content/pdf/10.1007/s12206-023-2105-y.pdf
Reference20 articles.
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2. L. Gao, X. Deng, X. Feng and Z. Yang, Effect of inlet conditions on compressor intermediate duct, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 229 (6) (2015) 1154–1168, https://doi.org/10.1177/0954410014542624.
3. W. K. Lord, G. L. Suciu, K. L. Hasel and J. M. Chandler, Engine architecture for high efficiency at small core size, AIAA SciTech Forum, 53rd AIAA Aerospace Sciences Meeting (2015) DOI:https://doi.org/10.2514/6.2015-0071.
4. P. Bansod and P. Bradshaw, The flow in s-shaped ducts, The Aeronautical Quarterly, 23 (2) (1972) 131–140.
5. A. M. K. P. Taylor, J. H. Whitelaw and M. Yianneskis, Developing Flow in S-Shaped Ducts, NASA Contractor Report 3759, NASA (1984).
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1. A study of the effect of curvature and pressure gradient on aerodynamics performance and turbulence structure of S-shaped compressor transition duct;Australian Journal of Mechanical Engineering;2023-07-05
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