subsonic

subsonic aerodynamics

亚速空气动力学

The two-dimensional axisymmetric subsonic-transonic-supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method.

摘要对一实验电弧加热式发动机二维轴对称亚跨超速流动进行了数值模拟，所采用的方法是矢裂算法。