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The absolute/convective instability of incompressible swirling flows and the temporalinstability of compressible swirling flows have been fully explored, whereas the absolute/convectiveinstability of compressible swirling fl.

从N-S方程出发,通过正则模方法,研究了超声速尾涡的绝对/对流不稳定性性质。

A method using CFD technology is used for accurate prediction of aerodynamic force and heat of air-breathing hypersonic vehicles.

对吸气式高超声速飞行器而言,物面热流和摩阻的准确预测对飞行器设计及安全十分关键。

Numerical experiments,including supersonic flow,subsonic flow and low speed flow,show that the al...

验证算例包括超声速、亚声速以及极低速情形的化学反应流场,计算结果表明基于预处理AUSM+格式发展的算法能够有效地用于全速域范围内化学反应流动问题的模拟。

It is greater than the standard velocity of sound in the direction of the motion of the room and smaller in the opposite direction.

在房间运动的方向上的声速比标准声速要大些,在相反的方向上则比较小些。

A multiminate layer vapor screen technique and force measurement technique for an unsteady flow in the intermitted wind tunnel is presented in this paper.

本文介绍在暂冲式三声速风洞中实现了非定常流动的多片光蒸汽屏显示技术和测力技术,并用这两项技术研究了亚声速时70°后掠三角翼模型俯仰振动的非定常流动现象,探讨了由于三角翼模型俯仰振动产生的涡结构与纵向气动力特性之间的相关关

In order to improve penetrativity of hypersonic missile and enable air-launched hypersonic cruise missile to penetrate with skip trajectory, a new approach of generating positive angle of attack during reentry phase of trajectory was proposed. Some key parameters of realizing skip trajectory were found out, and the effects of these parameters on ballistic performance were discussed.

为提高高超声速导弹的突防能力,使常规布局空中发射的高超声速巡航弹能采用跳跃式弹道突防,采用了在导弹再入段附加相应的正攻角产生气动升力的方法,找出了实现弹道起跳的关键参数,讨论了这些参数对弹道性能的影响。

The results show that for a supersonic shear layer without reaction, a disturbance can make the shear layer become unstable, this results in one vortex or more than one vortex. The combination and seperation of vortex can intensify the mixing. But it is not easy for supersonic reacting shear layer with exotherm to become unstable with disturbance, and the effect duration is very long.

结果表明,对完全气体的超声速剪切层流动,一定的激励方式能使原先较为稳定的剪切层流动变得不稳定,产生单涡或多涡结构,发生多涡间的合并,使混合加剧;但对于存在放热现象的反应超声速剪切层流动,外加激励方式不易使流动从稳定变为不稳定,而且外加扰动的作用特征时间也较长,实际应用前景不乐观。

It is the first time to calculate the near noise field with ray method, and replace the inhomogenous SSP in the vertical direction with constant SSP, while other models usually use Fast Field Program such as SARFRI to calculate the near noise field. This model increases the calculation speed about 100 times without decreasing much precision. It can meet the need of engineering.

首次采用射线模型计算噪声近场的贡献,并进一步用等声速代替有垂直分布的声速剖面,而其他模型通常采用诸如SARFRI等快速场程序计算近场的贡献;本模型的计算时间比其他模型的计算时间缩短了2个数量级,精度并未有明显损失,适合工程需要。

In view that the combustion efficiency and flame stability are affected by the interaction of flow and combustion, further systematical research on phenomena and mechanism of the interaction between flow and combustion in supersonic combustors is needed.

由于流动与燃烧的相互作用直接影响超声速燃烧室中的燃烧效率与燃烧稳定性,因此有必要对超声速燃烧室中流动与燃烧的相互作用现象及其机理进一步开展系统深入的研究工作。

The influence of the size of sound lens and the sound velocity in sound lens material and crude oil and rock stratum on the sphere of action is studied.

分析了声透镜尺寸及材料中的声速、原油及岩层中的声速对其传播距离的影响。

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