排序方式: 共有57条查询结果,搜索用时 15 毫秒
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As a main oxidizer in solid composite propellants, ammonium perchlorate (AP) plays an important role because its thermal decomposition behavior has a direct influence on the characteristic of solid com-posite propellants. To improve the performance of solid composite propellant, it is necessary to take measures to modify the thermal decomposition behavior of AP. In recent years, transition metal oxides and carbon-supported transition metal oxides have drawn considerable attention due to their extraor-dinary catalytic activity. In this review, we highlight strategies to enhance the thermal decomposition of AP by tuning morphology, varying the types of metal ion, and coupling with carbon analogue. The enhanced catalytic performance can be ascribed to synergistic effect, increased surface area, more exposed active sites, and accelerated electron transportation and so on. The mechanism of AP decom-position mixed with catalyst has also been briefly summarized. Finally, a conclusive outlook and possible research directions are suggested to address challenges such as lacking practical application in actual formulation of solid composite propellant and batch manufacturing. 相似文献
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随着时钟频率的增加以及电源电压的降低,电源完整性问题日益凸显。将电流变化率加入到最差噪声算法的电流约束中,能够在任意电流变化率的情况下分析电源分布网络的最差噪声,从而获得更加真实的最差噪声。另外,利用改进的Knuth-Yao四边形不等式法对基于动态规划的最差噪声算法进行加速,加速后算法的时间复杂度从O(n~2m)降为O(mnlogn)。 相似文献
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紊流混合摩擦区是成品油管输的基本流区,其摩阻因数的基准公式为科尔布鲁克公式,国标采用十分近似、容易计算的哈兰德公式。由于历史原因,前苏联学者阿尔特舒尔的紊流混合摩擦因数公式在我国石油储运界一直流行,但该式只适用于管径较小、管内壁较粗糙、雷诺数较低的情况,而科式和哈式没有这种限制,且后者的计算也很简单,故阿式应割爱停用。 相似文献
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航迹偏差的控制精度对滑跑起降至关重要,地面滑跑纠偏建模和地空航迹控制的切换策略是起降航迹控制设计的难点。从运动学关系出发,提出了地面滑跑纠偏控制的设计模型,使得复杂的地面航偏控制规律易于设计;利用同-反馈结构在多个状态的协调控制,实现了地空状态自然过渡的航迹控制切换策略;最后提出了提高航迹控制精度和进行风干扰补偿的措施。 相似文献
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This paper develops a panel smooth transition vector autoregressive model to investigate the economic growth–defense causality. This model simultaneously resolves the estimation problems of endogeneity, heterogeneity, and nonlinearity. Empirical results support that the causality is bidirectional, nonlinear, time- and country-varying. Economic growth has a negative impact on military spending and vice versa. The larger the HDI, the smaller the negative causality. Evidently, the increase in the level of country development can reduce the negative impact of military outlays on economic growth. Reducing the ratio of military spending to GDP is beneficial for countries with low HDI scores; however, moderately increasing the share of military expenditure is favorable for countries with extremely high HDI scores. Policy authority needs to set optimal education, health, and economic development shares of GDP for purchasing a maximum economic growth rate. 相似文献
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Andrew Phiri 《Defence and Peace Economics》2019,30(4):474-487
Using annual data collected from 1988 to 2015, this study provides evidence of a non-linear relationship between military spending, economic growth and other growth determinants for the South African economy. The empirical study is based on estimates of a logistic smooth transition regression (LSTR) model and our empirical results point to an inverted U-shaped relationship between military spending and economic growth for the data. Furthermore, our empirical results suggest that the current levels of military spending, as a component of total government expenditure, are too high in the South African economy and need to be transferred towards more productive non-military expenditure in order to improve the performance of economic growth and other growth determinants. 相似文献
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为了研究不同形状粗糙元诱导边界层转捩机理的差异,采用五阶精度加权紧致非线性格式数值模拟了Ma=4. 20条件下方柱形、圆柱形、钻石形和半球形粗糙元引起的超声速平板边界层转捩问题。结果表明:方柱形粗糙元产生的分离区长度较大,分离区中存在较强的非定常扰动并产生绝对不稳定机制使边界层很早就发生转捩;钻石形粗糙元分离区的展向宽度较宽,导致分离区中的涡结构向下游发展时形成的湍流尾迹区较宽;而圆柱形和半球形粗糙元诱导边界层转捩的能力相对较弱。 相似文献
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