空气动力学16.100 Aerodynamics |
|
课程网址: | http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-100-ae... |
主讲教师: | Prof. David Darmofal |
开课单位: | 麻省理工学院 |
开课时间: | 2005-01-01 |
课程语种: | 英语 |
中文简介: | 本课程将流体力学概念从统一工程扩展到亚超声速状态下机翼和物体的空气动力学性能。16.100 一般有四个组成部分: 亚音速势流, 包括源/涡旋面板方法;粘性流, 包括层流和湍流边界层;翼型和机翼的空气动力学, 包括薄翼型理论、提升线理论和面板方法/相互作用的边界层方法;和超音速和高超声速翼型理论。课程材料每年因设计问题的重点而异。 |
课程简介: | This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub/supersonic regimes. 16.100 generally has four components: subsonic potential flows, including source/vortex panel methods; viscous flows, including laminar and turbulent boundary layers; aerodynamics of airfoils and wings, including thin airfoil theory, lifting line theory, and panel method/interacting boundary layer methods; and supersonic and hypersonic airfoil theory. Course material varies each year depending upon the focus of the design problem. |
关 键 词: | 空气动力学; 飞机气动模式; 流量计算; 计算流体力学; 空气动力学分析; 超音速; 亚音速; 涡格法 |
课程来源: | 麻省理工大学公开课 |
最后编审: | 2024-05-28:chenjy |
阅读次数: | 57 |