Optimization of supersonic inlet configuration using reinforcement learning coupled with aerodynamic performance surrogate model

Aerospace Science and Technology 2026

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Authors: Fan Yang, Chen Kong, Cheng-Kun Lv, Zi-Ao Wang, Juntao Chang

DOI: 10.1016/j.ast.2026.112146

Cited by: 2

References: 38

Fields of Study & Subjects

Computational Fluid Dynamics and Aerodynamics Model Reduction and Neural Networks Turbomachinery Performance and Optimization

References 38