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Hypersonic的中国译典句库查询结果如下:
属类:法学专业-中国法律-导弹及相关物项和技术出口管制条例
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1 | (三)超音速(马赫数为 1.4 至 5)和高超音速(马赫数为 5 至 15)的风洞,但专门设计用于教学目的和试验区的尺寸(在内部测得的)小于 25 厘米的风洞除外 | (3)Wind-tunnel for supersonic (Mach 1.4 to 5)or hypersonic (Mach 5 to 15)speeds except those specially designed for teaching and those with the test area dimensions smaller than 25 cm (measured internally); | |
2 | Busemann进气道风洞实验及数值研究 | Experimental Investigation and Numerical Simulation of Hypersonic Busemann Inlet | |
3 | TVD格式与高超音速气动加热数值模拟 | TVD Scheme and Numerical Simulation of Aerodynamic Heating in Hypersonic Flows | |
4 | 超声速和高超声速横向喷流数值模拟 | Numerical Simulation of Supersonic and Hypersonic Jet Interactions | |
5 | 抽吸对高超声速进气道起动能力的影响 | Effect of Suction on Starting of Hypersonic Inlet | |
6 | 带进气道的隔离段流场实验研究与数值模拟 | Experimental and Numerical Investigation of Isolator Combined with Hypersonic Inlet | |
7 | 低密度超音速风洞大约开始发展于1960年。 | hypersonic wind tunnels operating at very low densities were developed starting in about 1960 | |
8 | 典型二元高超声速进气道设计方法研究 | Study of Design Method of Typical two-dimensional hypersonic Inlet | |
9 | 典型几何和流动参数对高超声速进气道性能的影响 | Effect of Geometry and Flow Parameters on Internal Compression Performance of Typical Two-Dimensional Hypersonic Inlets | |
10 | 二维非常规压缩型面超/高超声速进气道的设计概念 | Concept of a two-dimensional Supersonic/Hypersonic Inlet with a non-conventional Compression Wall | |
11 | 二元混压式高超声速进气道流场数值模拟 | Numerical Simulations of Hypersonic Inlet Flowfields in the Binary Mixed Compression | |
12 | 非结构网格的高超声速粘性MHD流场数值模拟 | Numerical Simulation of Hypersonic Viscous MHD Flows Based on Unstructured Meshes | |
13 | 非结构网格高超声速绕流数值模拟及涵道构型减阻特性分析 | Numerical Simulation for Hypersonic Flow on Unstructured Grid and Analysis of Drag Induction Effects on Channel-Configuration | |
14 | 非线性动态逆控制在高超飞控系统中的应用 | Application of Nonlinear Dynamic Inversion Control in Flight Control of Hypersonic Vehicle | |
15 | 辐射及化学非平衡流耦合场计算方法 | Numerical Simulation of Hypersonic Flow with Non-Equilibrium Chemical Reaction and Radiation | |
16 | 高超飞行器进气道/内流道流动特性试验 | Experimental Study of Flow Characteristics of Inlet/Internal Flowpath for a Hypersonic Flight Vehicle | |
17 | 高超声速侧压式模型进气道不起动特性分析 | Characteristic Analysis of Unstart Performance for Hypersonic Side-Wall Inlet Model | |
18 | 高超声速串联式组合动力装置方案 | Hypersonic Combined Cycle Engine Concept with Tandem Layout | |
19 | 高超声速弹丸头部气动热研究 | Research of Aerodynamic Heating for Head of Hypersonic Projectile | |
20 | 高超声速二方程湍流模型的数值模拟对比 | Comparison of two-equation Turbulent Models for Hypersonic Flow Simulations | |
21 | 高超声速二维进气道参数化设计方法初探 | Preliminary Investigation on Parametric Design Method of the two-dimensional Hypersonic Inlet | |
22 | 高超声速二维前体/进气道一体化优化设计研究 | Integrative Optimum Design and Research for Hypersonic Two Dimensional Forebody/Inlet | |
23 | 高超声速飞机纵向通道的多级模糊逻辑控制 | Longitudinal Multistage Fuzzy Logic Control for Hypersonic Vehicle | |
24 | 高超声速飞行器BTT非线性控制器设计与仿真 | Design and Simulation of BTT Nonlinear Controller for Hypersonic Vehicle | |
25 | 高超声速飞行器单周期飞行轨迹优化研究 | Optimization on a Period of Flying Orbit of Hypersonic Vehicle | |
26 | 高超声速飞行器飞行特性和控制的若干问题 | Several Problems of Flight Characteristics and Flight Control for Hypersonic Vehicles | |
27 | 高超声速飞行器后体/尾喷管一体化设计 | The Application of Genetic Algorithms to Afterbody/Nozzle Integrated Design of a Hypersonic Vehicle | |
28 | 高超声速飞行器后体喷管设计 | Nozzle Afterbody Design of Hypersonic Flight Vehicle | |
29 | 高超声速飞行器滑行航迹优化 | Optimization of Glide Trajectory for a Hypersonic Vehicle | |
30 | 高超声速飞行器-进气道一体化热流数值计算 | Hypersonic vehicle-inlet Integrated Aeroheating Simulation |