4.4 Review

Cold spray nozzle Mach number limitation

期刊

JOURNAL OF THERMAL SPRAY TECHNOLOGY
卷 11, 期 4, 页码 496-507

出版社

ASM INTERNATIONAL
DOI: 10.1361/105996302770348628

关键词

cold spray; numerical modeling; shock-particle interaction; supersonic flow

向作者/读者索取更多资源

The classic one-dimensional isentropic flow approach is used along with a two-dimensional axisymmetric numerical model to show that the exit Mach number of a cold spray nozzle should be limited due to two factors. To show this, the two-dimensional model is validated with experimental data. Although both models show that the stagnation temperature is an important limiting factor, the one-dimensional approach fails to show how important the shock-particle interactions are at limiting the nozzle Mach number. It is concluded that for an air nozzle spraying solid powder particles, the nozzle Mach number should be set between 1.5 and 3 to limit the negative effects of the high stagnation temperature and of the shock-particle interactions.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.4
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据