一类平面系统的定性分析

利用平面系统的定性理论 ,提供系统的全局分析 ,讨论了一类平面系统奇点的稳定性和极限环问题 ,给出奇点稳定和极限环唯一的充分条件     

Z6等变系统所有可能的相图

简单介绍了 Z6 等变系统的背景 ,利用微分方程的定性理论及分枝理论 ,求出有限平面奇点及无穷远奇点 ;通过特征值方法判断奇点类型 ;根据系统等变性及解的唯一性讨论了在参数空间里所有可能的相图 ,给出了具体的形式 ,一共五类十六个相图 .     

论复自治微分系统的奇点量

本文讨论一类复三次微分系统及其“能量”扰动系统的若干实定性问题在复域中的同一性,主要结果如下: ⅰ)具有两个对称轴的实平面三次全微分系统可通过一个复三次系统作统一研究,不同实系统的轨线是同一复系统的积分曲面簇与不同坐标平面的截线。 ⅱ)上述能量扰动系统的细焦点、具有细鞍点的分界线环以及通过积分曲面与临界型奇点(实的或复的)相联的极限环,它们的稳定性同样地依赖于相应的区域奇点量,它们的重次同样地由相应临界型奇点的阶数确定,而它们可能分枝出极限环的最大个数除了同样地取决于上述阶数外,还取决于通过该奇点的积分曲面与坐标平面的截线的闭分枝的分布情况。 ⅲ)对上述系统不与有限远奇点相联的极限环,引入了“多重环量”,得到了内外稳定性及分枝问题的判据。     

似梯度型系统的连结轨线

本文讨论Ｒｎ中似梯度型系统奇点的连结轨线．给出了存在连结轨线的一个判定准则;证明了当系统仅有的两个奇点分别为吸引子和排斥子时,连结轨线集是无界的开集．     

连结奇点轨线的存在性

本文给出了判定平面动力系统两个奇点的连结轨线存在性的一个准则。     

孤立块与连结轨线的存在性

用孤立块的概念,给出了连结平面动力系统2个奇点的轨线的存在性准则。     

一类平面齐次多项式系统的局部相图

平面系统在动力系统的研究中起着重要的和基础的作用．在实系数系统情况下,本文利用奇点指数和牛顿多边形方法,讨论了一类平面齐次多项式系统在其孤立点附近的相图,同时给出一些奇点稳定的充要条件．     

微分方程定性理论的某些问题(最近文献综述)

近年来微分方程定性研究的问题是数学文献中最普遍的题材之一。定性理论的基本概念,定理与方法成为解决许多物理与技术问题的基本概念与方法。对于从事非线性振动,无线电物理学,自动控制的学者来说,应用奇点附近积分曲线的动态与分布的定理,奇点的指数,极限环线的概念等已极为习惯了。广泛地应用了庞卡赖-班狄克生的理论及在变换下的不动点的勃劳威雨原理等。在这方面,如果说对于无线电物理的问题对于具有一次自由度的系统的性质的研究是平面上积分曲线     

极限环问题

1.研究极限环的重要性所谓极限环就是平面定常系的孤立闭轨线,它附近的轨线当 t→∞或-∞时都以螺旋状方式向它无限接近。H.Poincaré首先发现极限环是非线性系统所特有的一种轨线,并找到研究极限环的三种重要方法,即地形系法,后继函数法和小参数法。的确,就平面定性理论的观点看来,要搞清楚不可积分的一阶非线性方程的积分曲线的全局结构,那末研究极限环问题是有着非常重要的意义的。因为研究积分线的全局结构,无非就是要解决下面三个问题:1)奇点附     

含奇异线的广义KdV方程的行波解

研究了一个广义KdV方程的行波解,在行波变换下,该方程转化成含奇异线的平面系统,通过平衡点分析定性地得到不同参数条件下系统解的特性.特别的,由于相平面上的奇异线的存在,系统具有一些特殊结构的解,例如compactons、kink-compactons、anti-kink-compactons,给出了这些解的积分表达式,并且由椭圆函数积分求出了精确解.     

Embedding quasi laminar 1D flame profiles to model turbulent premixed combustion with a joint PDF method

A new model for turbulent premixed combustion is presented which is based on a joint velocity composition probability density function (JPDF) method. The key idea is a scale separation approach. The method combines the model by Bray, Moss and Libby [1] (BML) for premixed combustion with the flamelet approach for nonpremixed combustion. Here, a Lagrangian formulation of the BML model is considered. The progress variable used by the BML model becomes a computational particle property and its value is triggered by the arrival of the flame front at the particle's position. Similar as in the flamelet approach we assume that the smallest eddies are not small enough to disturb the reactive diffusive flame structure. To resolve the (embedded) quasi laminar flame structure, a flame residence time is introduced. With that residence time, the evolution of the particle composition, including enthalpy, can be determined from precomputed laminar 1D flames. The main challenge with this approach is to model the probability that an embedded flamefront arrives at the particle location, which is necessary to close the chemical source term. Numerical experiments of a turbulent premixed flame show good agreement with experimental data. (© 2008 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)     

Extended flamelet model and improved interaction of chemistry and turbulence for modeling partially premixed combustion with a joint PDF method

Turbulent combustion is commonly categorized into premixed, non-premixed and partially premixed combustion. For nonpremixed combustion simulations the laminar flamelet concept proved to be very valuable while for the more complex case of partially premixed combustion this model shows considerable deficiencies. Here, the classical laminar flamelet approach is extended to the partially premixed combustion regime. For that, the joint statistics of mixture fraction, scalar dissipation rate and a progress variable, calculated with a joint probability density function (PDF) method, is used to get the statistics of the compositions and of the chemical energy source term from pre-processed flame tables. This approach can be compared with the unsteady flamelet concept; the main differences consists of the way the progress variable evolution is computed and in the pre-computed flame tables. The progress variable describes the point of time a fluid parcel is consumed by a flame front. The fluid parcels are represented by computational particles, which are used for PDF methods. The pre-computed flame tables are computed from steady solutions 2D stabilized flames propagating into an unburnt mixture with varying mixture fraction. The corresponding position of a fluid particle in such a 2D laminar flame is determined by its mixture fraction and a burning time; both to be modeled for each computational particle in the PDF simulation. Numerical experiments of turbulent diffusion jet flames demonstrate that this approach can be employed for challenging test cases. (© 2008 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)     

Wall effect on determination of laminar burning velocity in a constant volume bomb using a quasi-dimensional model

In experiment, two optical and pressure-based methods are frequently used to evaluate laminar burning velocity of a combustible mixture. In the currently reported work, the pressure-based method was utilized to find the laminar burning velocity using the measurement of pressure variations during the combustion process in a spherical bomb and analyzing them through a multi-zone quasi-dimensional model. To check the results of the method, isooctane–air mixtures were used at equivalence ratios of 0.85 and 1.0 and initial pressures of 95 and 150 kPa with 343 K initial temperature. The time history of the bomb pressure during the combustion event, initial pressure and temperature, fuel type, and equivalence ratio were applied as input to a Fortran program written by the author based on the multi-zone combustion model; and, flame radius-time, flame speed, and laminar burning velocity at different pressures and temperatures were evaluated assuming spherical flame growth. The obtained results were compared with those of some other researchers and a reasonable agreement was observed. The wall effect on the laminar burning velocity at the end of the combustion process was clearly highlighted and a reliable range of burning velocity was distinguished. The results showed that the evaluated laminar burning velocity was not reliable at the late part of the combustion process due to possible local contact of flame front and the bomb wall, the wall effect on the reacting species, flow to small crevices, and the boundary layer effect.     

Level Set Methods in a Benchmark for Thermoacoustic Instabilities

Gas turbines can suffer from combustion instabilities and combustion driven oscillations. As a prestep a 3D benchmark tube geometry for the complicated interactions between acoustics and thermal heat release is investigated. For the representation of the flame surface a Level Set approach was chosen. The resulting model includes the impact of curvature on the laminar burning velocity as well as the potential flow field and underlying velocity fields due to vorticity and volume expansion across the flame front. The acoustic equations and the thermal heat release are coupled by the acoustic velocity which is also included in the flame model. A numerical simulation of this benchmark problem is presented as a first step toward optimizing or controlling the stability behavior of the system. (© 2006 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)     

Dynamics of coal dust flame acceleration: A feedback control model for unsteady flow

Several modeling concepts borrowed from control theory are employed to develop an algebraic and ordinary differential equations model for the dynamics of unsteady coal dust flame acceleration in a constant area duct closed at one end, e.g., in a coal mine tunnel. We are particularly concerned with modeling the feedback mechanisms which cause a coal dust flame to accelerate, leading to detonation. Previous experimental studies have been conducted on both coal dust flame propagation and on individual coal particle combustion. Based on the results, a physical model is proposed in which coal dust flame acceleration is entirely controlled, in a feedback fashion, by volatiles emission and their reaction. A control system model is developed that employs five well-stirred reactor subsystems with three feedback interaction mechanisms. The model consists of a leading shock wave, followed by a variable length volatiles emission region ahead of the flame, a fixed length burning region immediately behind the flame front, and a variable length exhaust region extending back to the closed end of the duct. The feedback mechanisms incorporated into the model include heat transfer and pressurization from the burning region to the volatiles emission region, and pressurization from the volatiles emission region to the turbulent mixing region behind the shock wave. Each well-stirred reactor is described by a system of algebraic and ordinary differential equations for the rate of change of conditions inside the reactor. Numerical simulation results reveal that, despite far-reaching simplifications (ordinary instead of partial differential equations, ideal gases insteady of two-phase flow, separation of volatiles emission and combustion, neglection of char burning), the model exhibits the fundamental dynamic properties of the flame propagation process. The model agrees with qualitative photographic experimental results and is applicable to both the case where the flame accelerates to detonation and to the case where the combustion process dies out.     

Effects of Quadratic Singular Curves in Integrable Equations

In this paper, the effects of quadratic singular curves in integrable wave equations are studied by using the bifurcation theory of dynamical system. Some new singular solitary waves (pseudo‐cuspons) and periodic waves are found more weak than regular singular traveling waves such as peaked soliton (peakon), cusp soliton (cuspon), cusp periodic wave, etc. We show that while the first‐order derivatives of the new singular solitary wave and periodic waves exist, their second‐order derivatives are discontinuous at finite number of points for the solitary waves or at infinitely countable points for the periodic wave. Moreover, an intrinsic connection is constructed between the singular traveling waves and quadratic singular curves in the phase plane of traveling wave system. The new singular periodic waves, pseudo‐cuspons, and compactons emerge if corresponding periodic orbits or homoclinic orbits are tangent to a hyperbola, ellipse, and parabola. In particular, pseudo‐cuspon is proposed for the first time. Finally, we study the qualitative behavior of the new singular solitary wave and periodic wave solutions through theoretical analysis and numerical simulation.     

Global qualitative analysis of a quartic ecological model

In this paper we complete the global qualitative analysis of a quartic ecological model. In particular, studying global bifurcations of singular points and limit cycles, we prove that the corresponding dynamical system has at most two limit cycles.     

An Approach to Model Partially Premixed Turbulent Combustion withProbability Density Function (PDF) Methods

In turbulent combustion one distinguishes between premixed, non-premixed and partially premixed combustion. While laminar flamelet models proved to be extremely valuable for a wide range of non-premixed flame simulations, similar approaches are more problematic in the partially premixed regime. Here the laminar flamelet concept for non-premixed turbulent combustion simulations is generalized for the partially premixed regime. Similar as in the unsteady flamelet approach, the joint statistics of a progress variable, mixture fraction and scalar dissipation rate is used to obtain the joint statistics of the compositions from pre-computed flame tables. The required distribution is computed with a joint PDF method and the main differences between the new approach and previous ones, are the pre-computed tables and the way the evolution of the progress variable is calculated. Instead of evolving 1D flamelets, steady 2D solutions of burning flamelets propagating into unburned mixtures with varying mixture fraction are considered. The location of a fluid particle in this 2D laminar flame is defined by its mixture fraction and a burning time, which are modeled for each computational particle used in the PDF method. Numerical experiments of a turbulent lifted diffusion flame and a premixed Bunsen flame demonstrate that this approach can be employed for a wide range of applications. (© 2006 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)     

Modelling Intermediate Species in Partially Premixed Turbulent Combustion Based on the LES-FGM Method北大核心CSCD

The LES of partially premixed turbulent flame MRB in TU Darmstadt was conducted based on the flamelet-tabulated combustion model FGM, and effects of premixed and partially premixed tabulations on the modelling results were studied. The results show that, different methods of tabulation exhibit limited influences on the predictions of the flame structure, velocity, and major species, but using a partially premixed tabulation largely improves the reliability of modelling intermediate minor species CO and H2. The underlying reason lies in a better inclusion of the fuel-air mixing effects through the partially premixed tabulation, which is built based on laminar counter-flow flames. Adding extra transport equations for the intermediate species improves the predictions of intermediate species, especially given a premixed tabulation adopted; meanwhile, the stretch effects in this turbulent flame are ignorable. The results are significant to guide the high-fidelity simulation of partially premixed turbulent flames based on the flamelet-tabulated combustion model. © 2023 Editorial Office of Applied Mathematics and Mechanics. All rights reserved.     

A Lagrangian Joint PDF Approach for Turbulent Premixed Combustion

A model for premixed turbulent combustion based on a joint velocity probability density function (PDF) method and a progress variable is presented. Compared with other methods employing progress variables, the advantage here is that turbulent mixing of the progress variable requires no modeling. Moreover, by applying scale separation, the Lagrangian framework allows to account for the embedded, quasi laminar flame structure in a very natural way. The numerical results presented here are based on a simple closure of the progress variable source term and it is demonstrated that the new modeling approach is robust and shows the correct qualitative behavior. (© 2006 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim)