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Journal: Aerospace, 2025
Volume: 12
Number: 242

Article: Direct Numerical Simulation of Boundary Layer Transition Induced by Roughness Elements in Supersonic Flow
Authors: by Haiyang Wang, Zaijie Liu, Hexia Huang, Huijun Tan and Dan Zhao
Link: https://www.mdpi.com/2226-4310/12/3/242

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