Numerical Investigation of Active Flow Control of Blade Synthetic Jet on Performance and Stability of Transonic Axial Compressor Rotor
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-3998-1_44
Reference14 articles.
1. Braunscheidel, E. P., Culley, D. E., Zaman K.: Application of synthetic jets to reduce stator flow separation in a low speed axial compressor. In: 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008–602
2. Culley, D.E., Bright, M.M., Prahst, P.S., et al.: Active flow separation control of a stator vane using embedded injection in a multistage compressor experiment. J. Turbomach. 126(6), 24–34 (2004)
3. De Giorgi, M., Traficante, S., De Luca, C., et al.: Active flow control techniques on a stator compressor cascade: a comparison between synthetic jet and plasma actuators. ASME Paper, GT2012-69535 (2012)
4. Matejka, M., Popelka, L., Safarik, P., et al.: Influence of active methods of flow control on compressor blade cascade flow. ASME Paper, GT2008-51109 (2008)
5. Zander, V., Hecklau, M., Nitsche, W., et al.: Active flow control by means of synthetic jets on a highly loaded compressor cascade. Proc. IMechE Part A J. Power Energy 225(7), 897–906 (2011)
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