Spatial DNS of an Isothermal Flat Plate Supersonic Turbulent Boundary Layer with/out Impinging Shock Wave
Spatial direct numerical simulation results are presented for transitional/turbulent supersonic isothermal flat plate boundary layers at M = 2.0 and impinging shock wave-boundary layer interactions. The numerical results show the formation and development of three-dimensional vortical structures suc...
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| Autores principales: | , |
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| Formato: | Artigo |
| Lenguaje: | Inglês |
| Publicado: |
The Japan Society of Mechanical Engineers
2011-01-01
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| Colección: | Journal of Fluid Science and Technology |
| Materias: | |
| Acceso en línea: | https://www.jstage.jst.go.jp/article/jfst/6/1/6_1_30/_pdf/-char/en |
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