In this dissertation, detached-and large-eddy simulations are employed to study three typical flows including transonic flow past a circular-arc aerofoil, transonic flow past a sphere and a jet from a blunt body opposing a supersonic flow.
本文采用分离涡模拟和大涡模拟方法研究了三类典型流动问题,包括对称双弧翼型跨声速绕流、圆球跨声速绕流以及超声速来流下球柱体反向喷流。
参考来源 - 具有激波和湍流旋涡分离的可压缩绕流数值研究·2,447,543篇论文数据,部分数据来源于NoteExpress
A numerical method of computing steady supersonic flow fields by using adaptive streamline grids.
提出一个用自适应流线网格计算定常超声速流场的数值方法。
We present a method of analyzing flutter characteristics of wing with nonlinear stiffness in supersonic flow.
提出了带结构刚度非线性的超音速弹翼的颤振分析方法。
The ellipse arc may depress the acceleration of supersonic flow in inlet area, decrease the strength of inlet shock wave.
椭圆形的前缘可减弱超音气流在前缘进口区的加速程度,降低进口弓形波的强度;
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