Flow Control Effect of Spanwise Distributed Pulsed Arc Discharge Plasma Actuation on Supersonic Compressor Cascade Flow
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s11630-020-1382-3.pdf
Reference24 articles.
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4. John A., Qin N., Shahpar S., Using shock control bumps to improve transonic fan/compressor blade performance. Journal of Turbomachinery, 2019, 141(8): 081003.
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