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Receptivity and Forced Response to Acoustic Disturbances in High-Speed Boundary Layers
Supersonic boundary-layer receptivity to freestream acoustic disturbances is investigated by solving the Navier–Stokes equations for Mach 3.5 flow over a 7 deg half-angle cone. The freestream disturbances are generated from a wavy wall placed at the nozzle wall. The freestream acoustic disturbances...
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| Publicado no: | AIAA J |
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| Main Authors: | , , , , |
| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
2017
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| Assuntos: | |
| Acesso em linha: | https://ncbi.nlm.nih.gov/pmc/articles/PMC8051075/ https://ncbi.nlm.nih.gov/pubmed/33867531 https://ncbi.nlm.nih.govhttp://dx.doi.org/10.2514/1.J056145 |
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