• The problems of physical distortion due to the finite-difference scheme are studied in numerical solutions of the hypersonic viscous shock-layer equations.

    本文讨论了高超声速粘性激波层方程数值计算时差分格式引起的物理失真问题。

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  • The flexible coating is an energy conversion body that consists of confinement layer and Absorbing layer, so that laser shock processing(LSP) can be applied in engineering.

    柔性贴膜作为一种集约束层与吸收层于一体的新手段,使激光冲击技术有了更好的工程实际应用性。

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  • Laser shock hardening may change the structure and properties through forming shock wave and causing damage in the surface layer of metal.

    激光冲击硬化是通过在材料表层内形成冲击波而引起“损伤”来改变表层的组织和性能。

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  • We find that when the collapsing bubble approaches its minimum radius, a high pressure layer just outside the bubble is generated which gradually moves outward and subsequently forms a shock wave.

    计算还发现,当气泡接近它的最小半径处,气泡外围形成很薄的高压区,这个高压区域随后向外传播,这就形成冲击波。

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  • The relatively constant values of open circuit voltage suggest the electrolyte layer withstands thermal shock due to high thermal conductivity and excellent ductibility of the metal substrate.

    相对恒定的开路电压显示,电解质层经受住了热冲击,此受益于金属支撑体良好的导热性和延展性。

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  • An analysis of applicability and limitations of the method in the problems of shock layer stability on a flat plate are presented.

    对此法用于平板上激波层稳定性问题的适用范围和限制条件作了分析。

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  • The braid is used as an additional shield, which creates the shock-absorption layer beyond the jacket and at the same time is a bandage for the copper tapes screen.

    其纱辫充当除了护套外的防震缓冲层,同时又可以作为铜线和胶带间的绑带。

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  • In this paper, the nonequilibrium viscous shock layer equations have been used to calculate the hypersonic flows over blunt bodies in the fore-body region (including stagnation line and sonic line).

    本文从化学非平衡粘性激波层控制方程出发,用数值法计算了高超音速钝体绕流头部区流场(包括驻点线和音速线)。

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  • The ceramic layer does not crack or flake off when the composite pipe receives a mechanical shock.

    在受到一般性的机械冲击时,陶瓷层不碎、不裂。

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  • The failure wave phenomena in glass media under shock loading are analyzed. The propagating mechanism and dynamic characteristics of failure wave and the property of failure layer are revealed.

    分析了玻璃材料在高速冲击条件下的破坏波现象,对破坏波的传播机制及其动态特征以及破坏层的性质进行了研究。

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  • At present, there are two shock absorption measures of tunnel, namely shock absorption layer and aseismatic joint.

    目前隧道的减震措施主要有两种,即设置减震层和抗震缝。

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  • Chemical equilibrium is considered with the viscous shock layer equations.

    采用粘性激波层控制方程和平衡化学反应气体模型。

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  • It is shown by calculation and analysis that the main form of the interaction in compressor cascades is the interaction between shock wave and turbulent boundary layer in channels.

    作者经过计算和分析,说明压气机叶栅流中主要的相互作用形式是叶栅槽道中激波和湍流附面层的相互作用。

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  • One of the more severe fluctuating pressure environments encountered in supersonic or hypersonic flows is the shock wave oscillation driven by interaction of a shock wave with boundary layer.

    在超声速或高超声速绕流中,一种很严重的脉动压力环境是由激波边界层相互作用引起的激波振荡。

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  • Wall heat transfer fluctuations have been measured using a platinum film resistance thermometer in forward facing steps induced shock wave and turbulent boundary layer interaction fields.

    用铂膜电阻温度计测量了前向台阶诱导激波与湍流边界层相互作用流场中的表面热流率脉动。

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  • The chemical non equilibrium viscous shock layer flows over a teflon ablative wall are calculated numerically.

    本文对有泰氟隆烧蚀的化学非平衡粘性激波层流场进行了数值模拟。

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  • The internal flow fields in scramjet are very complex, due to the interaction of shock waves, expansion waves, boundary layer and strong reactions.

    超燃冲压发动机的内部流场很复杂,存在激波、膨胀波、附面层和剧烈的化学反应等相互作用,给数值模拟带来很大的困难。

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  • However, no thorough investigation has been made on shock wave boundary layer interaction in compressor cascades and only a few papers on this topic have been published.

    然而迄今为止,尚未深入进行过压气机叶栅激波附面层相互作用的研究,发表的文献极少。

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  • Secondly, the shock solutions as the shock layer near the boundary and interior of the interval are studied.

    其次,研究了当激波在区间的边界附近和内部的激波解。

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  • This paper presents the surface characteristics of the inter-action between shock wave and turbulent boundary layer induced by sharp fin with emphasis on Mach number effects.

    本文介绍了尖前缘翼诱导激波和湍流边界层干扰流场壁面特性,着重强调马赫数影响。

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  • It has been confirmed by experiments that the boundary layer suction can efficiently eliminate the separation due to interaction of a reflected shock wave with the wall boundary layer.

    实验证实了边界层抽吸可以有效地减小激波与壁面边界层相互作用所产生的分离现象。

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  • A heavy-duty foam layer helps absorb motion and shock from the sleep surface, enhancing firmness and durability.

    重量级特制海绵层,有效吸收体重的冲击力及震荡,提升床垫的耐用度及承托力。

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  • Secondly, shock layer corrective term near the interior point in the interval is constructed via the transformation of stretched variable.

    利用伸长变量,在区间内点附近构造问题解的激波层校正项;

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  • The shock response finite element model is established to simulate studying object which is a double-layer vibration isolation system of host machine in ship.

    以某船主机双层隔振系统为对象,建立了有限元冲击响应模型。

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  • There exists a critical state as cooling in supersonic region of shock layer.

    超音速区内冷却存在临界状态。

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  • The mechanism of laser shock peening and application of the coating and limiting layer are studied.

    研究激光喷丸的机理及涂层和约束层的应用技术。

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  • In this paper, a new type of interaction of a moving shock with an unsteady boundary layer had been studied theoretically and experimentally.

    本文探讨了一种新的激波——非定常边界层相互干扰现象。

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  • In this paper, a new type of interaction of a moving shock with an unsteady boundary layer had been studied theoretically and experimentally.

    本文探讨了一种新的激波——非定常边界层相互干扰现象。

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