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Ze-Yang Zhao

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Oct 2026

Multistage Enhanced Intelligent Aerodynamic Design Method for Hypersonic Forebody/Inlet Integration

The aerodynamic design of hypersonic forebody/inlet integration systems represents a challenging multiobjective optimization problem characterized by high-dimensionality, strong coupling, and expensive evaluations. To move beyond conventional empirical approaches, this paper introduces a knowledge-driven intelligent de...

Yue Ma, Ye Tian, Ze-Yang Zhao et al. · 0 citations

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