two dimensional inlet

基本解釋

The maximum total pressure recovery is an important factor in optimal integrated design of two-dimensional scramjet inlet.
在飛行器前體進(jìn)氣道的一體化優(yōu)化設(shè)計(jì)中，最大總壓恢復(fù)系數(shù)是一個(gè)必須考慮的參數(shù)。
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.
針對(duì)一種帶放氣槽的定幾何二元倒置“X”型混壓式超音速進(jìn)氣道進(jìn)行了風(fēng)洞吹風(fēng)實(shí)驗(yàn)。
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.
采用二維磁流體動(dòng)力學(xué)（MHD）模型對(duì)加速器模式的磁控進(jìn)氣道進(jìn)行了數(shù)值模擬和參數(shù)優(yōu)化。
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