two dimensional inlet

基本解释

The maximum total pressure recovery is an important factor in optimal integrated design of two-dimensional scramjet inlet.
在飞行器前体进气道的一体化优化设计中，最大总压恢复系数是一个必须考虑的参数。
A fixed-geometry two-dimensional mixed-compression supersonic inlet with sweep-forward high-light and bleed slot in an inverted "X"-form layout was tested in a wind tunnel.
针对一种带放气槽的定几何二元倒置“X”型混压式超音速进气道进行了风洞吹风实验。
The two-dimensional MHD controlled inlet in the accelerator mode is numerically simulated, and the influence of some key parameters on the performance of the inlet is analyzed.
采用二维磁流体动力学（MHD）模型对加速器模式的磁控进气道进行了数值模拟和参数优化。
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