Numerical Study of Dual Sweeping Jet Actuators for Corner Separation Control in Compressor Cascade
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-019-1231-4.pdf
Reference24 articles.
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3. Ma H., Li B., Effects of axial non-uniform tip clearances on aerodynamic performance of a transonic axial compressor. Journal of Thermal Science, 2008, 17(4): 331–336.
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5. Li L.T., Song Y.P., Chen F., Meng R., Flow control of bowed compressor cascades by vortex generator jet at different incidences. Journal of Aerospace Engineering, 2017, 30(5): 04017028.
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