上海航天（中英文）2025，Vol.42Issue(z1)：52-61,10.DOI:10.19328/j.cnki.2096-8655.2025.S1.007
星舰气动力/热特性数值计算与分析
Numerical Calculation and Analysis of Aerodynamic/Thermal Characteristics of Starship
摘要
Abstract
This paper investigates the aerodynamic characteristics of SpaceX's Super Heavy-Starship system through numerical simulations at varying flight altitudes and angles of attack,analyzing surface pressure distribution,skin friction coefficient,and heat flux patterns.The study employs the finite volume method to solve the Navier-Stokes equations with an implicit time-advancement scheme.Key findings reveal that as the angle of attack increases,high-pressure and high-skin-friction regions progressively shift toward the Starship's aft section,while heat flux intensifies markedly at the nose and control surface edges.Shock wave dynamics critically influence surface pressure and thermal load distribution.At an extreme 80° angle of attack,large-scale separated vortex structures on the leeward side significantly complicate aerodynamic behavior.The research provides theoretical support for optimizing the Chinese launch vehicle's thermal protection system,refining reentry trajectory control,and enhancing flight stability.关键词
高超声速/大攻角飞行/数值仿真/气动力特性/气动热特性Key words
hypersonic/high angle of attack flight/numerical simulation/aerodynamic characteristics/aerothermodynamic characteristics分类
航空航天引用本文复制引用
武天赐,袁震宇,白宏阳,靳科锐..星舰气动力/热特性数值计算与分析[J].上海航天（中英文）,2025,42(z1):52-61,10.基金项目
国家自然科学基金资助项目(12302376,U21B2028) （12302376,U21B2028）
江苏省自然科学基金资助项目(BK20230905) （BK20230905）
中央高校基本科研业务费专项资助项目(30923011033) （30923011033）
