Secondary flow in compressible turbulent flow through a square duct with an adiabatic wall
The compressible turbulent flows through a square duct including an adiabatic bottom-wall with three Mach numbers, M = 1,1.5,2 are investigated using the direct numerical simulation. The secondary flows, which are caused by the turbulent anisotropic effects, are drastically changed with respect to t...
| Main Authors: | , |
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| Format: | Article |
| Language: | Japanese |
| Published: |
The Japan Society of Mechanical Engineers
2015-06-01
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| Series: | Nihon Kikai Gakkai ronbunshu |
| Subjects: | |
| Online Access: | https://www.jstage.jst.go.jp/article/transjsme/81/827/81_15-00283/_pdf/-char/en |