当前位置：
X-MOL 学术
›
Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.
›
论文详情
Our official English website, www.x-mol.net, welcomes your feedback! (Note: you will need to create a separate account there.)
Systematic reduced order model development of a pitching NACA0012 airfoil
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.1 ) Pub Date : 2020-08-04 , DOI: 10.1177/0954410020946912 Jaclynn Mohrfeld Halterman 1, 2 , Mesbah Uddin 1
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.1 ) Pub Date : 2020-08-04 , DOI: 10.1177/0954410020946912 Jaclynn Mohrfeld Halterman 1, 2 , Mesbah Uddin 1
Affiliation
Simple reduced order models (ROMs) for the aerodynamic coefficients - lift, drag, and pitch moment - of a pitching NACA0012 airfoil are presented. The ROMs are designed for quick computation of the...
中文翻译：
俯仰NACA0012翼型的系统降阶模型开发
介绍了俯仰 NACA0012 翼型的气动系数（升力、阻力和俯仰力矩）的简单降阶模型 (ROM)。ROM 设计用于快速计算...
更新日期：2020-08-04
中文翻译：
俯仰NACA0012翼型的系统降阶模型开发
介绍了俯仰 NACA0012 翼型的气动系数（升力、阻力和俯仰力矩）的简单降阶模型 (ROM)。ROM 设计用于快速计算...
京公网安备 11010802027423号