1) three-dimensional sidewall hypersonic inlet
三维侧压式高超声速进气道
1.
Analysis of drags trait in three-dimensional sidewall hypersonic inlet
三维侧压式高超声速进气道阻力特性分析
3) hypersonic side-wall inlet
高超声速侧压式进气道
1.
The flow in a typical hypersonic side-wall inlet is analyzed with a three-dimensional numerical analyer.
对某典型高超声速侧压式进气道三维流场进行了数值分析 ,就壁面压力分布、波系结构和近壁流谱图与实验结果进行了比较 ,计算反映了流动的基本特征。
4) three dimensional supersonic intake
三维超声速进气道
1.
According to the design method of a typical three dimensional supersonic intake,a kind of three dimensional flow-path of a ram-rotor was designed.
借鉴典型三维超声速进气道的设计方法,设计了一种旋转冲压压缩转子三维进气流道,并采用三维雷诺平均N-S方程和Spalart-Allmaras湍流模型对其流场进行了数值研究。
5) three-dimensional sidewall inlet
三维侧压式进气道
1.
Investigation of drag reducing in three-dimensional sidewall inlet
三维侧压式进气道的减阻研究
6) hypersonic inlet
高超声速进气道
1.
Experimental investigation on the starting characteristics of a hypersonic inlet with moving entrance door;
开启式高超声速进气道启动性能试验
2.
Effect of suctions on maximum backpressure ratios of hypersonic inlets;
抽吸对高超声速进气道抗反压能力的影响
3.
Numerical simulations of hypersonic inlet flowfields in the binary mixed compression;
二元混压式高超声速进气道流场数值模拟
补充资料：高超
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参考词条