摘要
系统阐述了超音速混合气流场的特性及求解过程。针对复杂流场求解过程中有限元模型的建立、边界条件的确定以及求解过程的具体实现等进行了深入的理论分析和探讨。本文最后给出了一个运用FLUENT软件求解超音速气流场的实例。
This paper systematically introduces the property and resolving process of super-sonic mixed gas fluent field.It is discussed deeply that how to bulid the finite element models and decide the constrained boundary.Meanwhile,this paper also analysis the concrete resolving process.At last,an example which resolves super-sonic gas fluent field wiht FLUENT software is given.
出处
《航空计算技术》
2001年第1期19-21,43,共4页
Aeronautical Computing Technique
