hypersonic flow
英 [ˌhaɪpə(ː)ˈsəʊnɪk fləʊ]
美 [ˌhaɪpərˈsɑnɪk floʊ]
网络 高超音速流动; 高超声速流动; 高超声速流
双语例句
- It is also shown that the analytical solution to the case for hypersonic flow over a blunt nose body with smooth boundary is possible.
文中还指出了对高超音速绕流光滑边界问题解析求解是可能的。 - The thermal environment of the wedge leading edge is rigorous in hypersonic flow.
高超声速气流条件下，尖楔前缘的热环境非常恶劣。 - Analysis of the Scattering Characteristic for the Hypersonic Flow Field with Near Wake Region of Sphere
高超声速圆球绕流流场及其近尾尾迹流场电磁散射特性分析 - The direct problem of hypersonic flow past blunt bodies at small angles of attack
超音速（波）测速仪高超音速钝体小攻角绕流的直接问题 - Stability Characteristics of the Boundary Layer of an Axisymmetric Blunt Nosed Cone in the Supersonic and Hypersonic Flow
超声速高超声速球锥绕流的边界层稳定性特点初探 - Numerical simulation of weakly ionized gas hypersonic flow under uniform magnetic field
均匀磁场中高超声速弱电离气体流动数值模拟 - Through ground test and hypersonic flow research, he made great progress in air-breathing hypersonic technology.
通过地面试验和高超声速非平衡流的研究，取得了再入突防气动物理的重要进展。 - Analysis of the scattering characteristic for the hypersonic flow field of semi-sphere
高超声速半球绕流流场电磁散射特性分析 - Numerical analysis of inviscid equilibrium and non-equilibrium hypersonic flow past small blunt-nosed cones
小钝头锥无粘平衡、非平衡绕流流场的数值分析 - Schlieren visualization and processing of the boundary layer transition image on a cone in the hypersonic flow
高超音速流场中锥体边界层转捩图象的纹影显示及处理 - The new algorithm is used for the tomographic reconstructions of the density distributions in rocket exhausted jet and hypersonic flow, and some errors of the reconstruction result are discussed.
应用该算法，对火箭燃气射流场和高超音速流场的莫尔偏折图进行了处理和计算，重建出流场截面的密度分布，并对重建结果进行了分析。 - The effect of heating on flow ing in hypersonic flow
高超音速流动中热对流动影响的研究 - Numerical simulation for hypersonic flow of nonequilibrium gases around the Apollo command module
绕Apollo飞船的高超声速化学非平衡流动的数值模拟 - The paper widens the application of local method which used to be utilized in rarefied flow to the quick prediction of aerodynamic characteristics of missile-like reentry vehicle in hypersonic flow.
本文将计算高超声速稀薄气流过渡领域中气动特性的局部方法，推广应用到连续介质中弹头型高超声速再入飞行器气动力特性的快速估算。 - This paper presents a numerical analysis of inviscid equilibrium and nonequilibrium hypersonic flow past blunt-nosed slender cones.
本文给出钝头细长锥无粘、平衡和非平衡高超声速绕流流场的数值分析。 - The Application of Gas Self Luminosity in Hypersonic Flow Field Visualization
气体自发光在高超声速流场显示中的应用 - The nature of an open separation has been analysed qualitatively and the numerical simulation has been made for the hypersonic flow with an open separation over the blunt cone at angle of attack.
本文定性分析了开式分离的性状，并对钝锥有攻角超声速绕流的开式分离作了数值模拟。 - Using the color changing information of phase change paint, this technique mainly applies an image capturing and processing system which consists of a CCD video camera and a computer to measure the characteristic parameter and the heat transfer rate of model surface in hypersonic flow.
该技术主要是运用CCD摄像机与计算机组成的图像采集与处理系统，利用涂料发生相变的颜色变化信息，测定高超声速流场中模型表面气动加热的特性参数和热流分布情况。 - Computational results agreed with experimental data, and the viscous Cartesian grid can simulate hypersonic flow around complex configurations well.
计算表明，三维非结构贴体直角网格的粘性求解，可以适应各种高超声速的复杂外形，计算结果与试验吻合较好。 - Using the engineering methods of supersonic and hypersonic flow or local piston theory developed in this paper to compute unsteady aerodynamic loads, and coupling structural equations, the supersonic or hypersonic aeroelasticity with a typical servo system under thermal environment is simulated in time-domain.
运用超音速、高超音速气动力工程计算方法和本文发展的当地流活塞理论计算非定常气动力，耦合结构运动方程，实现了热环境中带有伺服机构的气动弹性的时域仿真。 - Numerical methods for hypersonic flow with chemical non-equilibrium reactions on the unstructured grid are used to analyze the drag induction of channel-configurations.
在非结构网格上对二维高超声速化学非平衡粘性绕流进行了数值模拟，并应用此方法对涵道构型高超声速减阻特性进行了数值分析。 - Thus it was extensively applied to experimental research of transonic and hypersonic flow.
因此，它在跨声速和超声速流的实验研究中得以广泛地应用。 - Application of Local Method in Quick Prediction of Aerodynamic Characteristics of Reentry Vehicle in Hypersonic Flow
高超声速再入飞行器气动特性的快速预示&局部方法的推广应用 - Turbulent separation features induced by blunt fins in hypersonic flow
钝缘舵高超音速湍流分离特性 - On the mathematical simulation of nonequilibrium hypersonic flow around the flying vehicle
关于飞行器高超声速不平衡气体绕流的数值模拟 - On Shock Layer Method for the Hypersonic Flow Problems
关于高超声速绕流问题的激波层方法 - This method is especially good for measuring unsteady hypersonic flow field. An integrated measuring system LVG-1 has been devel-oped.
这种方法特别适合于高超音速非定常流场，已研制成完整的测量系统LVG-1。 - Experiment research about lateral jet in hypersonic flow
高超声速侧向喷流干扰气动特性试验研究 - Study of heating protection features by mass injection over the local structure in a hypersonic flow
高超声速流中局部构件上质量引射的热防护特性研究 - A typical characteristic of hypersonic flow is the high temperature, which makes the air being decomposed and ionized, and local plasma flow formed around the aircraft, so the hypersonic flowfield is much more complicated than common flowfield.
高超声速流场的一个显著特点是高温下气体发生离解和电离，形成局部的等离子体流动，使得高超声速流场的结构变得很复杂。