说明:双击或选中下面任意单词,将显示该词的音标、读音、翻译等;选中中文或多个词,将显示翻译。
您的位置:首页 -> 句库 -> 超声速进气道
1.
Numerical Simulation of External-Compression Supersonic Inlet Flow Fields
外压式超声速进气道流场的数值模拟
2.
Design and Experimental Verification of Hypersonic Inlet with Rectangular Section
矩形截面高超声速进气道气动设计及实验验证
3.
Numerical Simulation and Experiment of Integral Flow Field of Diverterless Supersonic Inlet/Forebody
无隔道超声速进气道/前机身一体化计算与试验
4.
Numerical Simulation and Experimental Research of Hypersonic Inlet;
超声速进气道流场数值模拟与试验研究
5.
Design Method, Numerical Simulation and Experimental Research of Hypersonic Inlet;
超声速进气道的设计、计算与实验研究
6.
Effect of aspect ratio on 2-D hypersonic inlet performance
宽高比对二元高超声速进气道性能的影响
7.
Study of Optimization Method for Two-Dimensional Hypersonic Inlet
二维高超声速进气道优化设计方法研究
8.
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
9.
Impact of suction position on starting of hypersonic inlet
抽吸位置对高超声速进气道起动性能的影响
10.
Design for Throat Length of Mix-Compression Supersonic Inlet with Numerical Analysis
混压式超声速进气道喉道长度的设计与数值研究
11.
Calculation of Additive Drag of Supersonic Inlet under Subcritical Operating Condition
超声速进气道在亚临界条件下的附加阻力的计算
12.
Research on Numerical Simulation for Integrated Flow Field of Supersonic Inlet and Combustor;
弹用超声速进气道/补燃室流场及其一体化数值模拟研究
13.
Experimental Investigation of Fixed-geometry Two-dimensional Mixed-compression Supersonic Inlet with Twin-inlet 90° Configuration at Venter
双下侧定几何二元混压式超声速进气道的风洞试验
14.
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
15.
Effects of turning angles of wedge on unstart/restart characteristics of hypersonic inlets
楔面转折角对高超声速进气道不起动/再起动特性的影响(英文)
16.
Numerical Simulation of Supersonic Axisymmetric Inlet Flow Field
超声速轴对称进气道流场的数值模拟
17.
Study of Inlets/body Aerodynamic Interference of Supersonic Tactical Missile Using Numerical Simulation;
超声速战术导弹进气道/弹身气动干扰数值研究
18.
Supersonic chin inlet/airframe integration design
超声速下颔式进气道/前机身一体化方案设计