分层介质中散射体的声波衍射

Z. Nazarchuk, O. Ovsyannikov, R.V. Drogobytsky
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引用次数: 0

摘要

研究作用于散射体系统的场的性质是现代物理学的一个重要问题。在谐振频率范围内,当波的长度接近散射体的尺寸时,只有对相应的衍射问题进行严格的解,才有可能描述这种现象。在任意散射体几何形状的情况下,计算散射场会遇到很大的困难。本文提出了一种解决分层介质中散射体的标量声波衍射问题的方法。让平面xOy形成涂层(声速c1,介质密度l)与空气的介质界面。在声速为cz,介质密度为p的情况下,涂层与基材之间的平面y=-dis界面。横截面为l, k=m的圆柱形裂纹系任意位于平行于z轴的带材上。我们假设弧L,是任意曲率的李雅普诺夫型轮廓。具有标量分量(在xOy平面上)的二维自身结构模式(时间相关exp(-iot))激发了所呈现的结构。将出现的作用问题简化为二维亥姆霍兹方程的解,该方程满足以下条件:压力和速度矢量法向分量在下面的连续性;没有从无限远处传播的波(除了激发波);在弧线L, k = n和上平面上的Dirichlet;在散射体肋(Lk弧端点)附近,M为r型。采用Green - h - t - n方法,将初始问题求解为单层势。在满足散射体轮廓的条件下,将问题简化为一个积分方程组,用机械正交法求解为Nazarchuk[1]。注意,积分方程的核是由索默菲尔德型积分组成的,它们的计算应该小心。为此,我们提出修改积分路径以避免远区积分振荡。考虑到我们考虑一个自模激励,我们引入了透射系数和反射系数,并计算了下半空间耗散的耗散能。由此得到的问题的格林函数及其在远区行为的研究,使我们能够有效地求解该问题,并加强对该问题在大范围参数范围内的数值求解。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Sonic wave diffraction on scatterers in stratified medium
hvestigation of properties of fields, -acted on a system of scatterers, is an important problem of modem physics. Description of such phenomena m resonance fkequency range, where length of the wave close to the scatterers' dimensions, is possible only with a rigorous solution of corresponding diffraction problem. The significant difficulties arise while the scattered field is calculated in the case of an arbitrary scatterers' geometry. One of the ways to solve the problem of scalar sonic wave difEaction on scatterers in stratified medium is proposed below. Let the plane xOy forms the medium interface between coating (sonic wave velocity c1 and medium densitypl) and air. The plane y=-dis interface between coating and substrate with sonic wave velocity cz and medium density p,. A system of cylindrical W t e l y thin cracks with cross-section of L , k=m is arbitrary situated in the strip parallel to Oz-axis. We assume the arcs L, are the Lyapunov type contours of arbitrary curvature. Two-dimensional own mode of structure (time dependence exp(-iot)) with a scalar component (in plane xOy) excites the presented structure. The appeared =action problem is reduced to find the solution of twodimensional Helmholtz equation, that satisfies conditions: of continuity of pressure and normal component of velocity vector on the lower plane; of absence of waves propagated fiom infinity (except exciting one); of Dirichlet on the arcs L, k = n and on the upper plane; of M e h e r type near the scatterers' ribs (Lk arc end-points). Green h c t i o n method is used and a solution of initial problem is presented as siagle layer potential. Satismg condition on scatterers' contours the problem is reduced to system of integral equations that is salved by the mechanical quadrature method as Nazarchuk [l]. Note, the kernels of integral equations consist Sommerfeld type integrals and their calculation should be carem. For that purpose we propose to modify the integration path to avoid integrand oscillations at far zone. Taking into account we consider an own mode excitation, we introduce the coefficients of transmission, reflection and calculate dissipation energy that is dissipated in lower halfspace. Thus obtained Green function of the problem and its behaviour investigation at far zone allow us to solve effectively the problem and to enhance the solution to explore numerically the problem for wide range of its parameters.
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