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Xue-Qiang Liu

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Conference Open access Sep 2026

Aerodynamic characteristics of a reusable rocket at a representative supersonic recovery condition

This study investigates the aerodynamic characteristics of a reusable rocket under a representative supersonic recovery condition of H = 28 km and M = 2.2. Numerical simulations are conducted to examine the effects of angle of attack, control-surface deflection, and nozzle jet location on the aerodynamic forces, moment...

Yao Wu, Xue-Qiang Liu · 0 citations

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