本文介绍了一种涡格方法，它适用于亚声速飞机的纵横向气动特性计算。
This paper presents a vortex lattice method which is suitable for the calculation of subsonic longitudinal and lateral aerodynamic characteristics of aircraft.
本文探讨了超声速平板横向喷流干扰湍流流场的数值模拟方法。
A numerical method of the supersonic turbulent flow on the flat plate interacted by supersonic lateral jet is presented in this paper.
本文设计了三种频率的CO2激励射流，将其横向注入马赫数2.5的均匀超声速来流当中。
The CO2 jet excited under three different frequencies was injected into the Mach 2.5 supersonic flow.
本文设计了三种频率的CO2激励射流，将其横向注入马赫数2.5的均匀超声速来流当中。
The CO2 jet excited under three different frequencies was injected into the Mach 2.5 supersonic flow.
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