域F（z）上线性有源网络状态方程的存在性

如何将线性有源网络的每一支路上的物理参量都视为独立参量，那么，网络成了这些参量的有理函数域Ｆ（ｚ）上的网络；本文讨论了这样的网络在Ｆ（ｚ）上状态方程存在的充分条件。由于这条件只与网络的结构有关，因此使用十分简便。     

光参量振荡器在CARS测温技术中的应用

通过理论分析和实验结果，叙述了在宽带单脉冲相干反斯托克斯拉曼散射（ＣＡＲＳ）光谱测温技术中，利用光参量振荡器（ＯＰＯ）代替常用的染料激光器作为斯托克斯光源的可行性问题。理论分析指出，测温范围在２２００Ｋ以内，用ＯＰＯ作斯托克斯光源是可行的，并利用该实验装置实测酒精灯火焰中的温度分布，其结果与辐射温度计测量结果比较，误差在５％以内。     

新型波导缝隙天线反射特性的研究

本文根据等效源原理的分析了一种新型裂缝天线的反射特性，一个或两个横缝位于馈电矩形波导终端的短路面上。     

高速水下航行体超空化通气参数数值研究

超空化技术是水下航行体减阻增速的一种重要方式。通过求解N-S方程,利用两方程湍流模型和全空化模型对通气空化流场进行了数值模拟,研究了通气参数对空化流场结构的影响,揭示了通气超空化减阻机理和场内流动状况,分析了超空化航行体阻力特性,数值结果表明供气量是决定空泡形态和超空化航行体减阻效果的最关键因素,供气位置和方向对空泡形态及水动力特性的影响并不显著。     

某导弹发射箱箱盖开盖角度优化研究

采用求解三维、非定常、雷诺平均的N-S方程的方法,对某车载导弹发射过程中的燃气流场进行了非定常数值模拟。紊流模型采用标准的k-ε二方程模型,计算方法为有限体积法,计算网格为结构化网格。在此基础上研究了箱盖受力与开盖角度之间的关系,给出了最优开盖角度。     

Dynamic Study on Rigid and Flexible Coupling System for Terminally Sensitive Submunition

A kinetic model of the rigid and flexible coupling system for terminally sensitive submunition is set up with Kane＇s method. The parachute is considered as a flexible body, the flexible displacement is expressed with modal spread method, the position of the parachute is expressed with a hybrid coordinate method, and the kinematics of the terminally sensitive submunition is analyzed. Ten generalized coordinates relative to the attitude of the terminally sensitive submunition are chosen, and the correlative generalized active forces, the generalized inertial forces, the generalized internal forces are calculated in turn. On the base of the Kane＇s method, the ten degrees of freedom dynamic equations for the coupled terminally sensitive submunition are finally set up. This model can be used to expediently simulate and analyze accurately the exterior ballistic trajectory of terminally sensitive submunition, and provide the overall design of the terminally sensitive submunition with some helpful references.     

Improvement of the basic correlating equations and transition criteria of natural convection heat transfer

In this paper, improvements in the basic physical laws of natural convection heat transfer were implemented in two major respects by incorporating recent research findings in this field. A preferred transition criterion was adopted in this paper to correlate all of the experimental data. Since transition correlations are primarily flow stability problems, the Grashof number, instead of the Rayleigh number, was found to be the preferred criterion. Furthermore, in the case of natural convection heat transfer from a horizontal cylinder, a series of experimental data in the high‐Rayleigh‐number regions recently became available. These data made it possible to establish new reliable correlations and also to test the validity of previous correlations. It is concluded that the previous correlation for a horizontal cylinder in high‐Rayleigh‐number regions was based on unreliable experimental results. The transition correlation for a horizontal cylinder occurred at much higher values of Rayleigh number than the previous recommendation. In the case of natural convection heat transfer from a vertical plate, more accurate property values for air under pressurized conditions are now available. This made it possible to replot the reliable data of Saunders. From this result and the experimental result of Warner and Arpaci, a new set of basic correlations in natural convection heat transfer for laminar, transitional, and turbulent regimes are recommended. These recommendations reflect a better understanding of the basic physical laws in the field of heat convection. © 2001 Scripta Technica, Heat Trans Asian Res, 30(4): 293–300, 2001     

Transition prediction for a two‐dimensional reynolds‐averaged navier–stokes method applied to wind turbine airfoils

Boundary layer transition is significant to many flow fields that include both laminar and turbulent regions. Accurate prediction of transition onset is fundamental to the modelling of these flows. In most flow solvers based on the Reynolds‐averaged Navier–Stokes equations, transition onset must be specified manually. To overcome this weakness and to more accurately predict aerodynamic flow fields, a boundary layer transition prediction methodology is presented. This methodology, which has been applied to a Navier–Stokes solver, dynamically locates transition onset as the flow solution is converging. The prediction methodology identifies several boundary layer transition mechanisms, including Tollmien–Schlichting instability, laminar separation and turbulence contamination. Where possible, the implementation utilizes the calculated boundary layer velocity profiles to strongly couple the predicted transition locations and the flow solution. The transition prediction methodology was used to predicted transition onset for the NLF(1)‐0416 and S809 single‐element wind turbine airfoils. Results obtained with numerical calculations are found to agree well with experimental observations. Copyright © 2001 John Wiley & Sons, Ltd.     

倒灌河道水位流速计算方法研究

针对在大河倒灌情况下,如何确定跨越支流的桥梁设计桥高和桥下设计流速的问题,建立了基于完全圣维南方程组的水力学模型,通过物理模型试验,将所得结果配数学模型的计算结果加以比较,结果表明两者较为吻合,还给出了大河水位涨落时支流汇入大河处的最大流速的经验公式,对为数众多的中小河流的桥梁设计具有较好的参考作用。     

Nonhomogeneos Boundary-Value Problem for Semilinear Hyperbolic Equation. Stability

We discuss the solvability of the nonhomogeneous boundary-value problem for the semilinear equation of the vibrating string x _tt (t, y) − Δx(t, y) + f(t, y, x(t, y)) = 0 in a bounded domain and a certain type of superlinear nonlinearity. To this end, we deduce new dual variational method. Next, we discuss the stability of solutions with respect to the boundary control and initial conditions.