一类非线性奇摄动方程的激波问题

利用奇摄动理论和匹配原理，讨论了一类非线性奇摄动方程的激波问题．首先，构造了原问题的外部解和内层解．其次，研究了当激波在区间的边界附近和内部的激波解．最后，得出了与边界条件相对应的激波位置及解的表达式．     

一类拟线性边值问题的激波解

本文研究了一类拟线性边值问题的激波解，在适当的条件下，利用微分不等式理论，讨论了原边值问题激波解的存在性和渐近性态。     

边值对非线性方程激波解的影响

探讨了一类非线性方程奇摄动问题εy″ yy‘-x^ny=0,x∈（0,1),n≠-1,y(0)=α，y(1)=β的边界条件与激波解的关系，利用匹配条件得出了激波解存在的条件及对应的激波解。     

一类奇摄动非线性方程的激波解

利用匹配条件讨论一类奇摄动非线性方程激波解．得出了对应的激波解与边界条件的关系．     

p方程组的激波生成与构造

讨论p-方程组的激波生成与构造.精细地刻画了从光滑解到激波产生的转变过程,并给出了在激波生成点附近奇性结构与解的估计.     

Burgers方程的激波解与激波位置(英文)

讨论了Burgers方程激波解和位置的转移 .认为 :对该类方程 ,当边值发生微小变化时 ,不仅激波解发生变化 ,而且激波位置将发生较大的变化 ,甚至从内层移到边界 .其激波解也会发生相应的变化 .     

一类奇摄动边值问题的激波解

考虑了一个二阶奇摄动非线性边值问题,利用匹配展开法研究了该问题的激波解,并证明了问题的激波解的一致有效性.     

Burgers激波解的稳定性

本文探讨了在无究小扰动下Burgers激波解的稳定性,证明Burgers方程激波解在李亚普诺夫意义下是渐近稳定的.     

一类二阶奇摄动边值问题的激波解

考虑了一个二阶奇摄动非线性边值问题,利用匹配展开法研究了该问题的激波解,讨论了该问题的激波位置与边界条件的关系.     

用Lebesgue—Stieltjes积分定义的双曲型方程广义解

该文用Ｌｅｂｅｓｇｕｅ－Ｓｔｉｅｌｔｊｅｓ积分给出一个双曲型方程组广义解的新定义，在这个意义下证明了Ｃａｕｃｈｙ问题整体广义解的存在性。这种解自然地包含了δ－激波。     

非线性退化波方程的Riemann问题

研究了弹性力学中一退化波方程的Riemann问题．其应力函数非凸非凹,从而使得激波条件退化．通过引入广义激波条件下的退化激波,构造性地得到了各种情形下Riemann问题的整体解．     

一类非线性方程的激波解

该文是利用匹配条件讨论一类非线性方程激波解。得出了对应的激波解与边界条件的关系。     

一维非线性弹性力学方程组的Riemann问题

本文研究了一维非线性弹性力学方程组的Riemann问题.根据左右状态所处的相对位置,分情况构造了问题的唯一整体解.由于激波条件退化,系统的基本波除了稀疏波和激波还包含退化激波.     

The Riemann problem for general systems of conservation laws

An extended entropy condition (E) has previously been proposed, by which we have been able to prove uniqueness and existence theorems for the Riemann problem for general 2-conservation laws. In this paper we consider the Riemann problem for general n-conservation laws. We first show how the shock are related to the characteristic speeds. A uniqueness theorem is proved subject to condition (E), which is equivalent to Lax's shock inequalities when the system is “genuinely nonlinear.” These general observations are then applied to the equations of gas dynamics without the convexity condition P_vv(v, s) > 0. Using condition (E), we prove the uniqueness theorem for the Riemann problem of the gas dynamics equations. This answers a question of Bethe. Next, we establish the relation between the shock speed σ and the entropy S along any shock curve. That the entropy S increases across any shock, first proved by Weyl for the convex case, is established for the nonconvex case by a different method. Wendroff also considered the gas dynamics equations without convexity conditions and constructed a solution to the Riemann problem. Notice that his solution does satisfy our condition (E).     

Stability of a supersonic flow past a wedge with adjoint weak neutrally stable shock wave

We study the classical problem of a supersonic stationary flow of a nonviscous nonheat-conducting gas in local thermodynamic equilibrium past an infinite plane wedge. Under the Lopatinski? condition on the shock wave (neutral stability), we prove the well-posedness of the linearized mixed problem (the main solution is a weak shock wave), obtain a representation of the classical solution, where, in this case (in contrast to the case of the uniform Lopatinski? condition—an absolutely stable shock wave), plane waves additionally appear in the representation. If the initial data have compact support, the solution reaches the given regime in infinite time.     

On global transonic shocks for the steady supersonic Euler flows past sharp 2-D wedges

In this paper, under certain downstream pressure condition at infinity, we study the globally stable transonic shock problem for the perturbed steady supersonic Euler flow past an infinitely long 2-D wedge with a sharp angle. As described in the book of Courant and Friedrichs [R. Courant, K.O. Friedrichs, Supersonic Flow and Shock Waves, Interscience, New York, 1948] (pages 317-318): when a supersonic flow hits a sharp wedge, it follows from the Rankine-Hugoniot conditions and the entropy condition that there will appear a weak shock or a strong shock attached at the edge of the sharp wedge in terms of the different pressure states in the downstream region, which correspond to the supersonic shock and the transonic shock respectively. It has frequently been stated that the strong shock is unstable and that, therefore, only the weak shock could occur. However, a convincing proof of this instability has apparently never been given. The aim of this paper is to understand this open problem. More concretely, we will establish the global existence and stability of a transonic shock solution for 2-D full Euler system when the downstream pressure at infinity is suitably given. Meanwhile, the asymptotic state of the downstream subsonic solution is determined.     

星系螺旋结构的气体激波理论

本文用星际气体自引力星系激波来解释星系的螺旋结构、恒星的扰动引力场并非必要条件.我们首先证明,即使扰动引力场为零,也可以存在局部的星系激波解.这种解要求|ω_η0|>α,而且只要气体的密度反差比较大,就只能用激波解来解释螺旋结构.用叠代的方法求出了星际气体的自引力激波宏图.对一种特定的扰动引力场模拟气体自引力,可以在速度平面上定性分析激波解的特性.初始原星系盘中的物质分布不均匀性,通过缠卷过程、不稳定性增长和波动叠加.可以发展成星系激波宏图.这样,对星系激波的起源,演化和维持给出一个完整的图象.利用这个图象,可以解释星系螺旋结构的大量观测结果和分类特性.     

Analysis on linear stability of oblique shock waves in steady supersonic flow

An attached oblique shock wave is generated when a sharp solid projectile flies supersonically in the air. We study the linear stability of oblique shock waves in steady supersonic flow under three dimensional perturbation in the incoming flow. Euler system of equations for isentropic gas model is used. The linear stability is established for shock front with supersonic downstream flow, in addition to the usual entropy condition.     

Stability of transonic shocks for the full Euler system in supersonic flow past a wedge

We study the stability of transonic shocks in steady supersonic flow past a wedge. It is known that in generic case such a problem admits two possible locations of the shock front, connecting the flow ahead of it and behind it. They can be distinguished as supersonic–supersonic shock and supersonic–subsonic shock (or transonic shock). Both these possible shocks satisfy the Rankine–Hugoniot conditions and the entropy condition. We prove that the transonic shock is conditionally stable under perturbation of the upstream flow or perturbation of wedge boundary. Copyright © 2005 John Wiley & Sons, Ltd.