Parallel Large-Eddy Simulation of Subsonic and Transonic Flows with Transition in Compressor Cascade

What is it about?

Laminar-turbulent transition plays a critical role in the aerodynamic performance of compressors and is sensitive to flow conditions and external disturbances. This study is the first attempt to investigate the effects of free-stream turbulence on the mode and location of laminar-turbulent transition in the compressor cascade under both subsonic and transonic conditions using the LES method.

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