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 -> 高超声速进气道
1.
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
2.
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
3.
Numerical Simulation and Experimental Research of Hypersonic Inlet;
高超声速进气道流场数值模拟与试验研究
4.
Design Method, Numerical Simulation and Experimental Research of Hypersonic Inlet;
高超声速进气道的设计、计算与实验研究
5.
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
6.
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
7.
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
8.
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
9.
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)
10.
Investigation of a Two-dimensional Mixed-compression Hypersonic Inlet
一种高超声速二元混压式进气道的研究
11.
Experimental Study of Integrated Inlet/Internal Flowpath for an Airbreathing Hypersonic Vehicle;
吸气式高超声速飞行器前体进气道/内流道流动特性研究
12.
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
13.
Numerical Simulation of Supersonic Axisymmetric Inlet Flow Field
超声速轴对称进气道流场的数值模拟
14.
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
15.
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
16.
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
17.
Influence of blunted-lip cowl on performance of supersonic mixed-compression inlet
钝化唇缘对超声速混压式进气道性能的影响
18.
An Investigation of Stable Operation Range in Supersonic Axisymmetric Inlet
超声速轴对称进气道稳定工作范围研究