Ortega A López, Lombardini M, Hill D J
Graduate Aerospace Laboratories, California Institute of Technology, Pasadena, California 91125, USA.
Phys Rev E Stat Nonlin Soft Matter Phys. 2011 Nov;84(5 Pt 2):056307. doi: 10.1103/PhysRevE.84.056307. Epub 2011 Nov 14.
We present an approximate description of the behavior of an elastic-plastic material processed by a cylindrically or spherically symmetric converging shock, following Whitham's shock dynamics theory. Originally applied with success to various gas dynamics problems, this theory is presently derived for solid media, in both elastic and plastic regimes. The exact solutions of the shock dynamics equations obtained reproduce well the results obtained by high-resolution numerical simulations. The examined constitutive laws share a compressible neo-Hookean structure for the internal energy e=e(s)(I(1))+e(h)(ρ,ς), where e(s) accounts for shear through the first invariant of the Cauchy-Green tensor, and e(h) represents the hydrostatic contribution as a function of the density ρ and entropy ς. In the strong-shock limit, reached as the shock approaches the axis or origin r=0, we show that compression effects are dominant over shear deformations. For an isothermal constitutive law, i.e., e(h)=e(h)(ρ), with a power-law dependence e(h) is proportional to ρ(α), shock dynamics predicts that for a converging shock located at r=R(t) at time t, the Mach number increases as M is proportional to log(1/R), independently of the space index s, where s=2 in cylindrical geometry and 3 in spherical geometry. An alternative isothermal constitutive law with p(ρ) of the arctanh type, which enforces a finite density in the strong-shock limit, leads to M is proportional to R(-(s-1)) for strong shocks. A nonisothermal constitutive law, whose hydrostatic part e(h) is that of an ideal gas, is also tested, recovering the strong-shock limit M is proportional to R(-(s-1)/n(γ)) originally derived by Whitham for perfect gases, where γ is inherently related to the maximum compression ratio that the material can reach, (γ+1)/(γ-1). From these strong-shock limits, we also estimate analytically the density, radial velocity, pressure, and sound speed immediately behind the shock. While the hydrostatic part of the energy essentially commands the strong-shock behavior, the shear modulus and yield stress modify the compression ratio and velocity of the shock far from the axis or origin. A characterization of the elastic-plastic transition in converging shocks, which involves an elastic precursor and a plastic compression region, is finally exposed.
我们依据惠特姆的激波动力学理论,给出了由柱对称或球对称汇聚激波处理的弹塑性材料行为的近似描述。该理论最初成功应用于各种气体动力学问题,目前已推导至固体介质的弹性和塑性状态。所获得的激波动力学方程的精确解很好地重现了高分辨率数值模拟的结果。所研究的本构关系在内能(e = e(s)(I(1)) + e(h)(\rho, \varsigma))方面具有可压缩的新胡克结构,其中(e(s))通过柯西 - 格林张量的第一不变量考虑剪切作用,(e(h))表示作为密度(\rho)和熵(\varsigma)函数的静水压力贡献。在激波接近轴或原点(r = 0)时达到的强激波极限情况下,我们表明压缩效应比剪切变形占主导。对于等温本构关系,即(e(h) = e(h)(\rho)),具有幂律依赖关系(e(h))与(\rho^{\alpha})成比例,激波动力学预测对于在时间(t)位于(r = R(t))处的汇聚激波,马赫数随(M)与([\log(1/R)]^{\alpha})成比例增加,与空间指数(s)无关,其中在柱面几何中(s = 2),在球面几何中(s = 3)。具有反正切双曲正切类型(p(\rho))的另一种等温本构关系,在强激波极限下强制有限密度,对于强激波导致(M)与(R^{-(s - 1)})成比例。还测试了一种非等温本构关系,其静水压力部分(e(h))是理想气体的,恢复了惠特姆最初为理想气体推导的强激波极限(M)与(R^{-(s - 1)/n(\gamma)})成比例,其中(\gamma)与材料可达到的最大压缩比((\gamma + 1)/(\gamma - 1))固有相关。从这些强激波极限出发,我们还通过解析方法估计了激波后方紧邻区域的密度、径向速度、压力和声速。虽然能量的静水压力部分基本上决定了强激波行为,但剪切模量和屈服应力会改变远离轴或原点处激波的压缩比和速度。最后揭示了汇聚激波中弹塑性转变的特征,其中涉及弹性前驱波和塑性压缩区域。