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...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
The Japan Society of Mechanical Engineers
2011-01-01
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Series: | Journal of Fluid Science and Technology |
Subjects: | |
Online Access: | https://www.jstage.jst.go.jp/article/jfst/6/1/6_1_30/_pdf/-char/en |