Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV

Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV

Abstract Direct numerical simulation (DNS) of transition over a hypersonic lifting body model HyTRV developed by China Aerodynamics Research and Development Center is performed. The free-stream parameters are: the free-stream Mach number is 6, the unit Reynolds number is 10000/mm, the free-stream te...

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Bibliographic Details
Main Authors: Han Qi, Xinliang Li, Changping Yu, Fulin Tong
Format: Article
Language:English
Published: SpringerOpen 2021-10-01
Series:Advances in Aerodynamics
Subjects:
Lifting body model
Hypersonic transition
Direct numerical simulation
Online Access:https://doi.org/10.1186/s42774-021-00082-x

Internet

https://doi.org/10.1186/s42774-021-00082-x

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