Time-resolved phase-lock pressure-sensitive paint measurement of trailing edge noise dynamics
Author:
Funder
Japan Society for the Promotion of Science
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s00348-024-03838-5.pdf
Reference26 articles.
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2. Bertsch L, Snellen M, Enghardt L, Hillenherms C (2019) Aircraft noise generation and assessment: executive summary. CEAS Aeronaut J 10:3–9. https://doi.org/10.1007/s13272-019-00384-3
3. Bright A, Tichenor N, Kremeyer K, Wlezien R (2018) Boundary-layer separation control using laser-induced air breakdown. AIAA J 56:1472–1482. https://doi.org/10.2514/1.J055272
4. Crafton J, Stanfield S, Rogoshchenkov N, Schmit R (2017) Investigation of passive flow control of cavity acoustics using dynamic pressure-sensitive paint. In: AIAA SciTech forum—55th AIAA aerospace sciences meeting. https://doi.org/10.2514/6.2017-1178
5. Desquesnes G, Terracol M, Sagaut P (2007) Numerical investigation of the tone noise mechanism over laminar airfoils. J Fluid Mech 591:155–182. https://doi.org/10.1017/S0022112007007896
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