A Strongly-coupled Non-parametric Integral Boundary Layer Method for Aerodynamic Analysis with Free TransitionShun Zhang,Mark Drela,Steven R. Allmaras,Marshall C. Galbraith,David DarmofalAIAA Scitech 2019 Forum(2019)引用 3|浏览2AI 理解论文溯源树样例生成溯源树,研究论文发展脉络Chat Paper正在生成论文摘要