2) 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。
3) 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
4) 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
5) hypersonic inlets
高超声速进气道
1.
Characteristic analysis of unstart/restart of hypersonic inlets caused by variations of attack angle of freestream;
攻角引起的高超声速进气道不起动/再起动特性分析
2.
Effects of the forebody boundary layer state on flow structure and performance of hypersonic inlets;
前体边界层状态对高超声速进气道流动结构及性能的影响
3.
Effects of wall temperature on unstart/restart characteristics of hypersonic inlets
壁面温度对高超声速进气道不起动/再起动特性的影响
6) hypersonic forebody/inlet
高超声速前体/进气道
补充资料：高超
好得超过一般水平：见解～丨技术～。
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参考词条