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首页> 外文期刊>The Astrophysical journal >A NOZZLE ANALYSIS OF SLOW-ACCELERATION SOLUTIONS IN ONE-DIMENSIONAL MODELS OF ROTATING HOT-STAR WINDS
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A NOZZLE ANALYSIS OF SLOW-ACCELERATION SOLUTIONS IN ONE-DIMENSIONAL MODELS OF ROTATING HOT-STAR WINDS

机译:一维旋转热星风模型中加速解的喷嘴分析

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摘要

One-dimensional (1D) stellar wind models for hot stars rotating at approx> 75% of the critical rate show a sudden shift to a slow-acceleration mode, implying a slower, denser equatorial outflow that might be associated with the dense equatorial regions inferred for B[e] supergiants. Here we analyze the steady 1D flow equations for a rotating stellar wind based on a "nozzle" analogy for terms that constrain the local mass flux. For low rotation, we find the nozzle minimum occurs near the stellar surface, allowing a transition to a standard, CAK-type steep-acceleration solution; but for rotations approx> 75% of the critical rate, this inner nozzle minimum exceeds the global minimum, implying near-surface supercritical solutions would have an overloaded mass-loss rate. In steady, analytic models in which the acceleration is assumed to be monotonically positive, this leads the solution to switch to a slow-acceleration mode. However, time-dependent simulations using a numerical hydrodynamics code show that, for rotation rates 75%-85% of critical, the flow can develop abrupt "kink" transitions from a steep acceleration to a decelerating solution. For rotations above 85% of critical, the hydrodynamic simulations confirm the slow acceleration, with the lower flow speed implying densities 5-30 times higher than the polar (or a nonrotating) wind. Still, when gravity darkening and 2D flow effects are accounted for, it seems unlikely that rotationally modified equatorial wind outflows could account for the very large densities inferred for the equatorial regions around B[e] supergiants.
机译:对于以大约> 75%的临界速率旋转的热星,一维(1D)恒星风模型显示突然转变为慢加速模式,这意味着较慢,更密集的赤道外流可能与推断的密集赤道区有关B [e]超级巨人。在这里,我们基于“喷嘴”类比,对约束局部质量通量的项进行分析,以分析恒星旋转的稳定一维流动方程。对于低速旋转,我们发现喷嘴最小值出现在恒星表面附近,从而可以过渡到标准的CAK型陡加速解决方案。但是对于大约>临界速率的75%的旋转,此内部喷嘴最小值超过了整体最小值,这意味着近表面超临界解决方案将具有过载的质量损失率。在假定加速度为单调正数的稳定解析模型中,这导致解决方案切换到慢加速模式。但是,使用数值流体力学代码进行的随时间变化的模拟显示,对于临界转速的75%-85%而言,流量可能会从陡峭的加速度向减速的溶液发展出突然的“扭折”过渡。对于高于临界值85%的旋转,流体动力学仿真证实了缓慢的加速,较低的流速意味着密度是极风(或非旋转风)的5-30倍。尽管如此,当考虑到重力变暗和2D流影响时,旋转修改的赤道风流似乎不可能解释B [e]超巨星周围的赤道区域推断出的非常大的密度。

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