Mach 5 bow shock control by a nanosecond pulse surface dielectric barrier discharge
By M. Nishihara, K. Takashima, J. Rich, Igor V. Adamovich. 2011
159 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Radiology, Nuclear Medicine and Imaging
View Paper: https://www.semanticscholar.org/paper/7c6c54c3b9cd1d74c35f68fb2c6c4d3e2f6695e7
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In Aerospace Engineering
In Radiology, Nuclear Medicine and Imaging
Citations in the corpus
- Diagnostics for characterisation of plasma actuators (2015, background): “Their utilisation has been proposed, among others, for airfoil separation control [41–45], turbine blade separation control [46], laminar-turbulent transition delay [47], lift enhancement [48, 49], bluff body flow control [50, 51], shock wave control [52] and combustion augmentation [38].”