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121.
飞行模拟器上利用电动伺服加载系统替代传统的电液伺服加载后,需要进一步提高加载系统快速性、扩宽系统频带.建立了电动伺服加载模型,基于不变性原理对多余力矩进行补偿仍不能满足要求的情况下,利用模糊控制的快速响应特性,针对该系统设计出PI和模糊控制相结合的分段复合控制器.通过Matlab仿真结果表明使该系统既保证了控制无静差,静态稳定性好,同时动态性能有了较大提高. 相似文献
122.
A shock wave that is characterized by sharp physical gradients always draws the medium out of equilibrium. In this work, both hydrodynamic and thermodynamic nonequilibrium effects around the shock wave are investigated using a discrete Boltzmann model. Via Chapman–Enskog analysis, the local equilibrium and nonequilibrium velocity distribution functions in one-, two-, and three-dimensional velocity space are recovered across the shock wave. Besides, the absolute and relative deviation degrees are defined in order to describe the departure of the fluid system from the equilibrium state. The local and global nonequilibrium effects, nonorganized energy, and nonorganized energy flux are also investigated. Moreover, the impacts of the relaxation frequency, Mach number, thermal conductivity, viscosity, and the specific heat ratio on the nonequilibrium behaviours around shock waves are studied. This work is helpful for a deeper understanding of the fine structures of shock wave and nonequilibrium statistical mechanics. 相似文献
123.
The paper analyses the hydrodynamic instability of a flame propagating in the space between two parallel plates in the presence of gas flow. The linear analysis was performed in the framework of a two-dimensional model that describes the averaged gas flow in the space between the plates and the perturbations development of two-dimensional combustion wave. The model includes the parametric dependences of the flame front propagation velocity on its local curvature and on the combustible gas velocity averaged along the height of the channel. It is assumed that the viscous gas flow changes the surface area of the flame front and thereby affects the propagation velocity of the two-dimensional combustion wave. In the absence of the influence of the channel walls on the gas flow, the model transforms into the Darrieus–Landau model of flame hydrodynamic instability. The dependences of the instability growth rate on the wave vector of disturbances, the velocity of the unperturbed gas flow, the viscous friction coefficients and other parameters of the problem are obtained. It is shown that the viscous gas flow in the channel can lead, in some cases, to a significant increase in instability compared with a flame propagating in free space. In particular, the instability increment depends on the direction of the gas flow with respect direction of the flame propagation. In the case when the gas flow moves in the opposite direction to the direction of the flame propagation, the pulsating instability can appear. 相似文献
124.
125.
In this work, we used time-sliced ion velocity imaging to study the photodissociation dynamics of MgO at \mbox{193 nm}. Three dissociation pathways are found through the speed and angular distributions of magnesium. One pathway is the one-photon excitation of MgO(X\begin{document}$^1\Sigma^+$\end{document} ) to MgO(G\begin{document}$^1\Pi$\end{document} ) followed by spin-orbit coupling between the G\begin{document}$^1\Pi$\end{document} , 3\begin{document}$^3\Pi$\end{document} and 1\begin{document}$^5\Pi$\end{document} states, and finally dissociated to the Mg(\begin{document}$^3$\end{document} P\begin{document}$_\textrm{u}$\end{document} )+O(\begin{document}$^3$\end{document} P\begin{document}$_\textrm{g}$\end{document} ) along the 1\begin{document}$^5\Pi$\end{document} surface. The other two pathways are one-photon absorption of MgO(A\begin{document}$^1\Pi$\end{document} ) state to MgO(G\begin{document}$^1\Pi$\end{document} ) and MgO(4\begin{document}$^1\Pi$\end{document} ) state to dissociate into Mg(\begin{document}$^3$\end{document} P\begin{document}$_\textrm{u}$\end{document} )+O(\begin{document}$^3$\end{document} P\begin{document}$_\textrm{g}$\end{document} ) and Mg(\begin{document}$^1$\end{document} S\begin{document}$_\textrm{g}$\end{document} )+O(\begin{document}$^1$\end{document} S\begin{document}$_\textrm{g}$\end{document} ), respectively. The anisotropy parameters of the dissociation pathways are related to the lifetime of the vibrational energy levels and the coupling of rotational and vibronic spin-orbit states. The total kinetic energy analysis gives \begin{document}$D_0$\end{document} (Mg\begin{document}$-$\end{document} O)=21645\begin{document}$\pm$\end{document} 50 cm\begin{document}$^{-1}$\end{document} . 相似文献
126.
紫外光引发环氧树脂的下行前线聚合行为 总被引:1,自引:0,他引:1
采用紫外光(UV)引发法研究了221型脂环族环氧树脂的下行前线聚合行为.探讨了光引发剂、热引发剂用量和预热温度等对聚合前线的推动速率Vf和前线引发时间ti的影响,并利用傅里叶变换红外光谱(FTIR)、热重(TG)和差示扫描量热(DSC)等对固化物结构和热性能进行了表征.研究结果表明,提高光引发剂浓度、热引发剂浓度或预热温度,均可提高聚合前线的推动速率Vf,缩短引发时间ti.采用该技术制备的环氧树脂固化物具有较好的均一性及热稳定性. 相似文献
127.
128.
The selection of the correct mixing rule for sound velocity in ideal liquid mixtures determines the interpretation of the sound velocity in real mixtures. This is especially important for the determination of apparent properties of solutes, such as their apparent compressibility. There are different approaches reported in the literature, and this article presents a new derivation of the mixing rule based on statistical mechanics. It is shown that the correlation of volume fluctuations between adjacent components has a crucial influence on the ideal mixing rule. 相似文献
129.
通过对贫燃条件下(燃料与空气化学计量比φ=0.60-0.80)的甲烷/一氧化碳/空气火焰结构进行数值模拟,研究燃料中一氧化碳添加量对层流燃烧速度、氮氧化合物的排放以及熄火拉伸率的影响.随着燃料中一氧化碳添加量的不断增加,层流燃烧速度有所下降,这与燃料中加入氢气产生的现象有所不同.为了解释这一现象,本文深入探讨了层流燃烧速度与H+OH浓度峰值之间的关系,结果表明,一氧化碳的增加导致H+OH浓度峰值呈线性下降,与层流燃烧速度下降趋势完全一致.随着一氧化碳的增加,氮氧化合物排放量有所下降.探讨了NO的生成机理,且由敏感性分析得到生成NO的重要反应,分析当一氧化碳量增大时,NO的浓度以及重要反应的NO生成率均下降.此外,利用数值模拟求解径向拉伸率,深入分析燃料中添加一氧化碳时拉伸率对贫燃火焰稳定性的影响.由计算结果得到熄火拉伸率,发现燃料中一氧化碳的添加在一定程度上能够增强火焰的稳定性. 相似文献
130.
A numerical study of hydrogen-enhanced liquefied petroleum gas (LPG) + air flames was presented. The variations of the adiabatic burning velocity in different conditions of combustion (?=0.7-1.4) were studied extensively. The hydrogen content in the fuel was varied from 0% to 45% and the dilution factor was from 21% to 16%. Since the major components of LPG are butane and propane, an appropriate chemical kinetic model must be chosen to solve the chemical reaction of C3 and C4 species. Validation of the chemical kinetic model against the fundamental combustion data was performed to insure accuracy. In addition, independent simulations were conducted in the opposed-jet, symmetric, twin-flame configuration. The effects of fluid mechanics, as manifested by the induced strain rate, were also considered. The effects of extinction strain rate on flame temperature and the flammability limits were calculated and the results showed that hydrogen-enhanced LPG/air premixed flames were more stable at high flame strain. The lean flammability limits were extended by the H2 addition. 相似文献