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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Bibliographic Details
Main Authors: Yusuke TOKURA, Hiroshi MAEKWA
Format: Article
Language:English
Published: The Japan Society of Mechanical Engineers 2011-01-01
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