2) axisymmetric inlet duct
轴对称进气道
1.
Preliminary design on variable-geometry axisymmetric inlet duct;
可变几何轴对称进气道初步设计
3) 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
4) 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
5) supersonic inlet
超声速进气道
1.
Design and wind tunnel test on supersonic inlet with boundary layer bleed;
超声速进气道边界层吸除方案设计及实验
2.
Numerical simulation and experimental verification of a fixed-geometry 2D mixed-compression supersonic inlet with sweepforward high-light and "X"-type missile configuration;
定几何二元倒置“X”型混压式超声速进气道数值仿真与实验验证
3.
Numerical simulation of compressible and incompressible flows in mix-compression axisymmetric supersonic inlet;
超声速进气道可压及不可压流动数值模拟
6) mixed-compression axisymmetric inlet
混压式轴对称进气道
补充资料：轴对称
也称“线对称”。如果把一一个图形沿着某一条直线折过来，它能与另一个图形重合，那么称这两个图形关于这条直线成轴对称。这条直线称为对称轴。如果两个图形关于某直线成轴对称，那么对应点的连线被对称轴垂直平分。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条