边界层转捩的数值模拟
Simulation of Boundary Layer Transition
-
摘要: 在数值模拟中将Abu-Ghannam&Shaw(AGS)转捩模型引入到湍流模型中,以考虑流动中的层流和转捩现象,并在此基础上,分别对低雷诺数情况下的平板和涡轮叶栅流动进行了模拟,并与实验结果进行了比较,表明加入转捩模型可以较好地描述边界层的转捩过程。同时,结果还表明AGS转捩模型对压力梯度变化较大情况下的模拟稍有偏差。Abstract: The Abu-Ghannam and Shaw (AGS) model was added to the turbulent model in order to simulate the process of laminar to turbulent transition.Flat plate and turbine cascade boundary layer was studied and compared to the experimental data.The results show that the transition process could be better simulated by the transition model,but the simulation shows little deviation from the test data under great change of pressure gradient.
-
Key words:
- aerospace propulsion system /
- boundary layer transition /
- flat plate /
- turbine /
- simulation
-
点击查看大图
计量
- 文章访问数: 1689
- HTML浏览量: 87
- PDF量: 460
- 被引次数: 0

下载: