- 更多网络例句与扩散喷管相关的网络例句 [注：此内容来源于网络，仅供参考]
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An adaptive grid scheme controlling cell area is used to generated grids in the divergent section of symmetric annular nozzle, and the generated grids are used in the flowfield calculation through the uncoupled way. The elliptic equations are used to generate grids in three dimensional regions of FDN divergent section, the source terms used in the equations employ a mathematical form which is independent of the boundary shape and of the boundary grid point distribution, the free parameters contained in the source terms are determined by the two restraint conditions, the intersection angle of transverse grid lines with boundaries and the local curvature of the transverse grid lines at the boundaries, and the interior grid distribution controlled directly by the grid point distribution assigned on the boundaries is realized, it makes the grid more clustering near the nozzle wall. For the generated grids in the whole computational regions have a good smoothness and orthogonality, the accuracy of calculation in the flowfield is ensured.
对轴对称的环形喷管采用控制网格面积的自适应网格方法对扩散段部分进行了网格生成，并通过非耦合方式应用于喷管的流场计算中；对强制偏流喷管扩散段内的三维区域采用椭圆型方程进行网格生成，方程中的源项采用了与边界形状和边界网格点分布无关的数学形式，源项内的自由参数由横向网格线与边界的交角及横向网格线在边界处的局部曲率两个约束条件来确定，实现了由边界上的网格分布直接控制内部的网格点，使壁面附近具有较密集的网格，并且在整个计算区域内的网格都具有良好的光滑性和正交性，从而保证了流场计算的准确性。
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Forced Deflection Nozzle is studied from two aspect of experiment and numerical calculation in this thesis....
本文从实验和数值计算两方面对强制偏流喷管扩散段内的流动进行了研究。
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On the basis of it, the pressures along the divergent section and on the plug base of the nozzle are measured, the work process of the divergent section is analysed according to the experimental results, and it is coincident with the qualitative analysis about the simplified model.
在此基础上又对喷管扩散段和底部的压力进行了测试，并根据实验结果对喷管扩散段的工作过程进行了分析，与简化模型的定性分析结果相一致。
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In order to design optimum nozzle for air-air missile solid rocket motor, the mass model of solid rocket motor, the nozzle specifice impulse model of solid rocket motor and the objective function are established. Five different type of nozzles are choosen lor calculation: Conical, parabolidal,two different arcs,quadiatic polynominal and cubic polynominal.
以两种空-空导弹固体火箭发动机喷管作为算例，为此，建立固体火箭发动机的质量模型，喷管的质量比冲模型和目标函数模型，选择五种喷管扩散段内型面：锥形喷管，抛物线喷管，双圆弧喷管，二次多项式喷管和三次多项式喷管，进行优化设计，利用优化理论，成功地完成了五个设计变量的优化问题。
- 更多网络解释与扩散喷管相关的网络解释 [注：此内容来源于网络，仅供参考]
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conation：意动 意志
con-dinozzle 收敛扩散形喷管 | conation 意动 意志 | conavesetting 凹板调节
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divergent nozzle：扩散喷管
cultivated species 栽培种 | divergent nozzle 扩散喷管 | livestock product 畜产品
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divergent nozzle：扩散形喷管
divergent flow 发散流 | divergent nozzle 扩散形喷管 | divergent series 发散级数
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efflux viscosimeter：流出式粘度计
efflux viscometer 射流粘度计 | efflux viscosimeter 流出式粘度计 | effuser 扩散喷管
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livestock product：畜产品
divergent nozzle 扩散喷管 | livestock product 畜产品 | special purpose 特殊用途[目的], 单一用途
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effusiometer：隙透计
effuser 扩散喷管 | effusiometer 隙透计 | effusion meter 流量计
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effusiometer：气体扩散计
effuser 喷管;扩散器;集气管 | effusiometer 气体扩散计 | effusion 喷发
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ZAR effuser：扩散器,喷管;漫射体;扬声器纸盒
efficiency, quantum 量子效率 | ZAR effuser 扩散器,喷管;漫射体;扬声器纸盒 | ejector 发射器,喷射器;抽气器