流体中文网第二届数值模拟大赛第九弹!
流体中文 网 第二 届数值 模 拟 大赛徐 慎 忍 id: flowinflow
February 2, 2015
同样,该题目也是由flowinflow提交的,至此,在作者允许公布的作品已经全部公布完毕,一段时间以后我们将公布比赛成绩,感谢大家对流体中文网的支持,感谢各位选手的辛勤劳动。
Flow condition:
• Mach number: 0.84
• Angle of attack: 3.06 o
• Reynold’s number: 2 × 10 7
The results from Fluent are in go o d agreement with b oth the results from NASA
WIND co de and the exp erimental results, despite the fact that the geometry
used in this work has a planar wing tip, while for the exp eriment and geometry
used by WIND co de, the wing tip is rounded (Fig.11). Since there flow is highly
three dimensional near the wing tip, why this difference in the wing tip shap es
do es not seem to have a strong effect on the sho ck lo cation is sub ject to further
investigation.
结果很漂亮作者很有水平!
很漂亮!欢迎各位网友参与评价。
很专业,很漂亮 小弟学习了
实验和模拟结果,基本重合了呀。
:lol,很酷。
图9太漂亮了!计算的真棒!
右边第二个这么像我以前画的呢
笑返 发表于 2015-4-15 11:12
右边第二个这么像我以前画的呢
哪一个?
很漂亮,不过纵坐标貌似是-CP
很漂亮,努力学习了
很赞!
好厉害:)
牛
厉害!{:3_46:}
干嘛不用自己的code做
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