首页> 外文OA文献 >Stationary structures of irrotational binary systems -- models for close binary systems of compact stars
【2h】

Stationary structures of irrotational binary systems -- models for close binary systems of compact stars

机译:非旋转双星系统的平稳结构-紧凑星的紧密双星系统的模型。

摘要

We propose a new numerical method to calculate irrotational binary systems composed of compressible gaseous stars in Newtonian gravity. Assuming irrotationality, i.e. vanishing of the vorticity vector everywhere in the star in the inertial frame, we can introduce the velocity potential for the flow field. Using this velocity potential we can derive a set of basic equations for stationary states which consist of (i) the generalized Bernoulli equation, (ii) the Poisson equation for the Newtonian gravitational potential and (iii) the equation for the velocity potential with the Neumann type boundary condition. We succeeded in developing a new code to compute numerically exact solutions to these equations for the first time. Such irrotational configurations of binary systems are appropriate models for realistic neutron star binaries composed of inviscid gases, just prior to coalescence of two stars caused by emission of gravitational waves. Accuracies of our numerical solutions are so high that we can compute reliable models for fully deformed final stationary configurations and hence determine the inner most stable circular orbit of binary neutron star systems under the approximations of weak gravity and inviscid limit.
机译:我们提出了一种新的数值方法来计算由牛顿重力中的可压缩气态恒星组成的非旋转二元系统。假设无旋性,即在惯性系中恒星中各处的涡度矢量消失,我们可以为流场引入速度势。利用这个速度势,我们可以得出一组稳态的基本方程,它由(i)广义伯努利方程,(ii)牛顿重力势的泊松方程和(iii)Neumann速度势方程组成类型边界条件。我们首次成功开发了一种新的代码来计算这些方程的精确数值解。在由引力波发射引起的两颗恒星合并之前,双星系统的这种无旋结构是由不粘气体组成的现实中子星双星的合适模型。我们数值解的精度非常高,因此我们可以为完全变形的最终静止构型计算可靠的模型,从而在弱重力和无粘极限的近似条件下确定双元中子星系统的内部最稳定的圆形轨道。

著录项

  • 作者

    Uryu K; Eriguchi Y;

  • 作者单位
  • 年度 1998
  • 总页数
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类

相似文献

  • 外文文献
  • 中文文献
  • 专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号