论文部分内容阅读
介绍一种三角翼的结构及特点,通过Fluent对空气有攻角扰流并发生边界层分离现象进行仿真分析。研究空气扰流三角翼的流动情况,并通过仿真分析得到可压缩外部扰流对三角翼的影响结果。
This paper introduces the structure and characteristics of a delta wing, and analyzes the disturbing phenomenon of the boundary layer by Fluent. The flow field of the spoiler is studied, and the effect of the compressible external spoiler on the delta wing is obtained through the simulation analysis.