Effects of nozzle-lip thickness on the tones in the near-field pressure spectra and on the initial instability waves of jets
Author:
Affiliation:
1. Ecole Centrale de Lyon
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3935
Reference53 articles.
1. SUPERSONIC JET SCREECH: HALF-CENTURY FROM POWELL TO THE PRESENT
2. Aeroacoustic resonance and self-excitation in screeching and impinging supersonic jets – A review
3. Receptivity characteristics of under-expanded supersonic impinging jets
4. A complex-valued resonance model for axisymmetric screech tones in supersonic jets
5. Nozzle external geometry as a boundary condition for the azimuthal mode selection in an impinging underexpanded jet
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