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Quantitative model for the generic 3D shape of ICMEs at 1 AU

机译:1 AU下ICME的通用3D形状的定量模型

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Context. Interplanetary imagers provide 2D projected views of the densest plasma parts of interplanetary coronal mass ejections (ICMEs), while in situ measurements provide magnetic field and plasma parameter measurements along the spacecraft trajectory, that is, along a 1D cut. The data therefore only give a partial view of the 3D structures of ICMEs. Aims. By studying a large number of ICMEs, crossed at different distances from their apex, we develop statistical methods to obtain a quantitative generic 3D shape of ICMEs. Methods. In a first approach we theoretically obtained the expected statistical distribution of the shock-normal orientation from assuming simple models of 3D shock shapes, including distorted profiles, and compared their compatibility with observed distributions. In a second approach we used the shock normal and the flux rope axis orientations together with the impact parameter to provide statistical information across the spacecraft trajectory. Results. The study of different 3D shock models shows that the observations are compatible with a shock that is symmetric around the Sun-apex line as well as with an asymmetry up to an aspect ratio of around 3. Moreover, flat or dipped shock surfaces near their apex can only be rare cases. Next, the sheath thickness and the ICME velocity have no global trend along the ICME front. Finally, regrouping all these new results and those of our previous articles, we provide a quantitative ICME generic 3D shape, including the global shape of the shock, the sheath, and the flux rope. Conclusions. The obtained quantitative generic ICME shape will have implications for several aims. For example, it constrains the output of typical ICME numerical simulations. It is also a base for studying the transport of high-energy solar and cosmic particles during an ICME propagation as well as for modeling and forecasting space weather conditions near Earth.
机译:上下文。行星际成像仪提供了行星际冠状物质抛射(ICME)最密集等离子体部分的2D投影视图,而原位测量则沿航天器轨迹(即1D切割)提供了磁场和等离子体参数测量。因此,数据仅给出了ICME的3D结构的部分视图。目的通过研究大量距离其顶点不同距离的ICME,我们开发了统计方法以获得ICME的定量通用3D形状。方法。在第一种方法中,我们从假设3D冲击形状的简单模型(包括扭曲轮廓)的理论上获得了冲击法线方向的预期统计分布,并将其兼容性与观察到的分布进行了比较。在第二种方法中,我们使用了冲击法线和通量绳轴方向以及冲击参数来提供整个航天器轨迹的统计信息。结果。对不同3D震荡模型的研究表明,这些观测结果与围绕Sun-apex线对称的震荡以及宽高比约为3的不对称震荡兼容。此外,靠近其顶点的平坦或浸入的震荡表面只能是少数情况。其次,沿ICME前沿,鞘层厚度和ICME速度没有整体趋势。最后,将所有这些新结果与以前的文章重新组合在一起,我们提供了定量的ICME通用3D形状,包括电击,护套和磁通绳的整体形状。结论。获得的定量通用ICME形状将对几个目标产生影响。例如,它限制了典型ICME数值模拟的输出。它也是研究ICME传播过程中高能太阳和宇宙粒子的传输以及对地球附近的太空天气状况进行建模和预测的基础。

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