Improved Γ-Reθ-ar Model for Predicting Distributed Roughness-Induced Transition
AIAA JOURNAL（2025）
关键词
Hypersonic Boundary Layer Transition,Heat Transfer,Ablative Materials,Hypervelocity Free Flight Aerodynamic Facilities,Computational Fluid Dynamics,Boundary Layer Transition,Hypersonics,Distributed Roughness
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